request for proposal (rfp) fabrication of ......sac-isro page 2 of 45 specifications for fabrication...
TRANSCRIPT
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REQUEST FOR PROPOSAL (RFP)
FABRICATION OF ORIGAMI LENS FOR
BANDS B1-B4
March 2019
SPACE APPLICATIONS CENTRE
INDIAN SPACE RESEARCH ORGANIZATION (ISRO)
AHMEDABAD – 380015
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SAC-ISRO Page 1 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
CONTENTS Section I Introduction 2
Section II Optical/mechanical/thermal requirements 5
Section III Specifications of front and rear surfaces of Origami lens 8
Section IV Final specifications of Origami lens 10
Section V Quality provisions 12
Section VI Test requirements 15
Section VII Documents required 18
Section VIII Deliverables and packaging 19
ANNEXUREs
ANNEXURE 1 Design / Sag Specifications 21
ANNEXURE 2 Coating / Black Paint On Lens - Specifications 25
ANNEXURE 3 Tolerance Specifications 35
ANNEXURE 4 References 36
ANNEXURE 5 Compliance Matrix for RFP 37
ANNEXURE 5 Mechanical Drawings 41
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SAC-ISRO Page 2 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION I
INTRODUCTION
1.1 Scope
After successful implementation of proof-of-concept models of 8-fold and 4-fold
origami lens, we extend the scope of the Origami lens activity for development of a 4-
band camera with IRS bands B1-B4. In this document, the procurement specifications
for fabrication and testing of four-fold Origami Lens for development of compact
camera system are given. This document specifies the details necessary for the design
and testing of the compact lenses.
The scope of the work includes:
Study of the specifications provided by SAC.
Procurement of the blanks required for fabricating Origami lenses.
Fabrication of four-fold lenses as per the specifications given in this document
Meeting the performance parameters as per the specifications / standards
Demonstration of the performance of the lenses as per the specifications.
Provide test data to SAC for dispatch clearance.
Packaging in a suitable container and shipment to SAC.
This document covers:
- A general description of Origami Lens - Optical specifications of the lens - Tolerance specifications - Required optical testing for quality assurance - Deliverables - Schedule
1.2 General description of Origami Lenses Taking advantage of both reflective and refractive optical systems, light is folded
multiple times in a single crystal for designing the camera optics with desired
performance. Light enters through an annular aperture and with the help of concentric
zone reflectors, it is focused at the image plane. Folding the light helps to achieve the
desired focal length without increasing the total optical track. To achieve desired
performance, aspheric surfaces are used which also help to minimize aberrations and
improve the design tolerances with increase in depth of focus of an optical system. With
folded optics, the region between reflectors can be cut into baffles and made absorbing
to reduce stray light effects.
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SAC-ISRO Page 3 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
The origami lens based camera system would be used for airborne applications.
A solid CaF2 geometry has been chosen to increase the achievable FOV, which is
limited by the reflective geometry. In contrast to the eight-reflection lens, the front and
back sides of the four-reflection lens are designed aspheric.
The lens is designed with 4-fold bi-aspheric surfaces having 67.5 mm focal length with
an overall clear aperture diameter of 65 mm and physical diameter of 70mm. This
obscured system has an effective aperture of 36.55mm and f-number of 1.85 which
covers ±6.8 degree field of view. Figure 1 shows a typical optical schematic of the lens.
Figure 1: Typical 2-D Optical Schematic of 4-fold lens
Detailed description for the development of the four-fold origami is given in the
following sections.
1.3 Applicable Documents
The latest revision of the following documents (including but not limited to) form a part
of specifications.
MIL-0-13830C - Optical components for fire control instruments: General
specification covering the manufacture, assembly and
inspection of
MIL-M-13508C - Mirrors, glass, front surfaces aluminized for optical
elements
MIL-0-16898 - Optical elements packaging
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SAC-ISRO Page 4 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
MIL-675C - Coating of glass elements (Anti-Reflection) MIL-C-48497 - Durability requirement for coating single or multilayer,
interference …
MIL-I-45208 - Inspection requirements
1.4 Test Sequence
The test sequence as given in this document shall be adhered to. No other additions,
deletions and/or alterations to the test sequence and/or test specifications shall be done
without formal approval from SAC (ISRO).
1.5 Conditions and methods of test
The test conditions shall be in accordance with the specifications given in this
document. The test methods and the measurement procedures shall be worked out by
the supplier and submitted to SAC (ISRO) for approval. In any case, the supplier has
no right to implement any changes in the conditions or methods of the test without
formal approval from SAC (ISRO).
1.6 Supplier’s responsibility
The supplier shall be responsible for fabrication and testing of the 4-fold lens as per the
relevant specifications within the performance limits in the scheduled timeline. The
supplier shall also be responsible for delivering the product safely to the SAC. Any
lapse on the part of this would be the responsibility of the supplier.
1.7 Inspection rights
SAC reserves the right to participate in and monitor any of the tests and inspections
called for in this document. The supplier shall submit a schedule of activities, including
major milestones to SAC.
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SAC-ISRO Page 5 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION II
OPTICAL/MECHANICAL/THERMAL REQUIREMENTS
Total 04 Origami lenses are to be fabricated by the vendor. Thereafter, based on SAC’s
feedback of coating qualification, supplier has to take up coating of lenses.
2.1 The following are the optical, mechanical and thermal requirements to be met
for realization of the multi-fold Origami lens.
High quality CaF2 glass with high material homogeneity shall be used for fabrication of Origami lenses. The physical/ mechanical/ thermal properties of
the material batch to be used shall be sent to SAC.
Proper stress relieving shall be carried out on the blanks. This is to ensure that there is no stress on the Origami lens during diamond turning and testing.
The manufacturer shall ensure that holding of the components does not induce any stresses and result in surface figure changes on removal of the component
from the fabrication/test fixtures. The manufacturer shall device suitable test
methods to demonstrate this aspect.
2.2 Scope of Work
Fabrication and testing of origami optics involves -
1. Study of optical design provided by SAC
2. Design of reflective coatings and providing response curves to SAC
3. Qualification of coating by vendor as per details specified in RFP
4. Fabrication of Origami lenses
5. Coating of lens elements as per SAC feedback
6. Black painting of optics as per the details specified in RFP
7. Testing to ensure compliance to the specifications provided
8. Preparing test reports and providing to SAC for review and approval
9. Dispatch of optics to SAC
Fabrication and testing should be carried out to the best of engineering practices.
2.3 Sequence of Activities
1. The supplier shall study the optical design provided by SAC. Supplier shall prepare
the work plan for fabrication, coating and testing of the optics. The work plan shall
be submitted to SAC for approval.
2. SAC shall have the right to carry out minor modifications in the optical design
before the fabrication starts at no extra cost.
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SAC-ISRO Page 6 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
3. Procurement of all optical glasses, thermal paint etc. shall be initiated immediately
on receipt of purchase order.
4. The melt values of procured CaF2 glass shall be provided to SAC as soon as they
become available to adjust melt values in the optical design.
All materials shall be procured in ONE lot and from the same batch.
5. Response plots (in excel sheet) for coating design is to be provided to SAC for
approval.
6. Coating trial runs to be made and testing to be carried out to ensure compliance to
appropriate MIL standards. Results of the coating runs to be provided to SAC along
with the coating witness samples.
7. Fabrication of optical components including black painting as required.
8. Dimensions of all fabricated parts to be provided to SAC for approval. All
dimensions should be measured very accurately, preferably, in 3D CMM.
9. Measured data (Radius of curvature, SAG) of individual zones to be provided to
SAC for approval.
10. Optical testing to be carried out by vendor as per details provided in RFP (sections
IV & VI)
11. Review of all measured data by SAC and compliance to the specifications.
12. Prepare proper packaging before dispatching the optics to SAC in suitable
containers.
2.4 Anti-reflection coating on the optical surfaces
The fabricator is responsible for the design and qualification of antireflection coatings
as per the relevant MIL / ISO standards. After qualification to MIL standards,
deposition of Anti-reflection coatings on optical surfaces (specified zones) is to be
carried out (refer Annexure 2). These coatings should minimize the surface reflection
(in the spectral range 350-1100 nm) to less than 0.4 percent on all surfaces. Design
reflectance curves and measurements on witness samples are to be provided to SAC.
Coating samples of ~25mm diameter, three (03) numbers shall be supplied to SAC
before actual coating of lenses.
2.5 Reflective Coating
Specified zones (refer annexure 2) shall be coated with metallic coatings (enhanced
Aluminium or Protective silver preferably). This coating should meet the reflectance
specifications given in Tables 3.1.12. The protective layer used shall be validated on
the substrate. The witness samples of the coatings shall be fabricated along with
hardware in conformity with relevant MIL – standards and shall be verified through
tests on witness samples. Reflectance measurements shall be carried out through CaF2
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SAC-ISRO Page 7 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
glass with 5 mm material thickness. Test conditions will be worked out by manufacturer
in consultation with SAC.
After coating qualification, deposition of coatings is to be carried out by vendor as per
the specifications provided in RFP. These coatings should maximize the surface
reflection in the spectral range of 400 - 900 nm. Average reflection should be more than
88% for all surfaces over the spectral range.
2.6 Black Painting
Lenses are to be black painted (at specified zones) to reduce stray light (refer annexure
2). The paint to be used should be vacuum compatible. Black painting details are
provided in annexure 2.
Two of the available products are:
Supplier 1 MAP, Z.I Rue Ciement Ader, 09100 Pamiers, France
Items: PU1 black paint (1 kg pack) + PU1 thinner (1 litre pack) + Phosmap 11
primer (1 litre pack) + Phosmap 11 thinner (1 litre pack) + middle
plywood box.
Supplier 2 Lord Corporation, Chemical products, 2000 West Grandview Blvd,
P.O. Box 10038, Erie, PA 16514, United States.
Items Aero glaze Z306 Quart + Aero glaze 995824a quart.
The black paint should be applied according to the instructions of the selected
manufacturer.
5 samples of 75mm x 75mm x 3 mm thick BK7 / CaF2 should be provided to SAC
before painting of actual lens cells, barrel and spacers. After getting clearance from
SAC, painting of lenses should be started.
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SAC-ISRO Page 8 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION III
SPECIFICATIONS OF FRONT AND REAR SURFACES
OF ORIGAMI LENS
3.1 To meet design specifications, a four-reflection lens design in CaF2 is optimized
in ZEMAX. Our four-reflection lens design, shown in Figure 1, is an annular
reflective lens utilizing four concentric aspheric reflectors to focus incoherent
light to an image plane in near alignment with the back-side of the lens.
This section gives the optical specifications of an Origami lens in table below.
The tolerances on each of these specifications are also given.
TABLE 3.1
Please refer to Annexures for details
SPECIFICATIONS OF 4-FOLD ORIGAMI LENS
Please refer to Figure 1 for drawing of this multi-fold lens
S.No. PARAMETER SPECIFICATION
1. Material CaF2
2. Surface As per the Surface Sag
specifications / ZEMAX® design
given in Annexure -1 for all 4
bands B1 – B4
3. Shape of the Lens Circular
4. Physical Diameter Between 70.00mm and 75.00 mm
5. Clear Aperture 65.00mm (Refer Annexure 1 and 2
for details)
6. Surface Profile Aspheric (Both at front and rear)
(Refer Annexure 1 and 2 for
details)
7. Circularity at Edges
Mounting Surface Finish
Within 1 micron
Shall be finished to Emery 303 (or
equivalent)
8. Chamfering Sharp edges of the lens shall be
chamfered to around 0.5mm
9. Surface Figure (Over the Full Active
Area) Better than /6 Peak-to-Valley
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SAC-ISRO Page 9 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
/35 RMS, → 632.8 nm (He-Ne)
10. Scratch/Dig 60/40 or better
11. Surface Roughness Less than 5 nm
12. Reflectance
At all Angles of Incidence
Enhanced Al Coating / Silver Coating
(mutually agreed upon) with an
additional Protective Overcoat over the
entire active area
Average ≥ 88%
(0.4 – 0.9 microns)
Measurement of reflectance to be
carried out through CaF2 glass with
5 mm thickness of material.
(refer section 2.5)
13. Coating Pinholes There should be no pinholes visible
in the coating when it is
illuminated by a bright source of
light / backlit (As per relevant MIL
standard)
14. Coated Area Please refer Annexure 2
15. Tolerance on Coated Area (For
S.No.14.)
±50 microns
16. Coating Thickness Uniformity Better than 1 percent (desirable)
17. Uncoated Area (Annular Aperture for
Light Input, Rear Central Portion for
Light Exit)
Please refer Annexure 2
18. Black Painted Area
Qualified black paint shall be used.
Please refer Annexure 1
19. Anti-Reflection Coating Anti-reflection coating on
uncoated area with less than 0.4%
reflection over spectral range 0.35
– 1.1 microns. (Please refer
Annexure 2 and section 2.4)
Note: The optics shall meet the required performance as stated in Table above for a thermal
environment of 20 ± 3°C. In addition to this, the system shall withstand a storage temperature
range from 10° C to 50°C.
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SAC-ISRO Page 10 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION IV
FINAL SPECIFICATIONS OF ORIGAMI LENS
4.1 This section gives the optical specifications as a complete lens after the
completion of fabrication through diamond turning process, coating and black paint.
These parameters will be tested by the fabricator and/or at SAC. It is to be ensured that
the specifications of the completed lens (after lens turning, coating and black painting)
meet the specifications mentioned in table 1.1 within the specified tolerance values
(Annexure 3).
In case, the numbers do not match within the given tolerances, the fabricator will have
to re-fabricate the lens to meet the desired specifications (in consultation with SAC).
The final specifications of the lens would be provided at the time of placement of the
purchase order.
The specifications are given in table 4.1 below. The ZEMAX listing is provided in
Annexure 1 for all the bands as mentioned in the RFP Document.
The lens has to be fabricated using single-point diamond turning machine on CaF2
material as per the specifications given in Section III, meeting the quality and
performance specifications as laid down in the RFP.
TABLE 4.1
SPECIFICATIONS FOR THE ORIGAMI LENS: LENS
PERFORMANCE PARAMETERS
S.No. PARAMETER SPECIFICATION
B1 B2 B3 B4
1. Effective Focal Length 67.5 mm ± 1 mm
2. F/Number (Effective) 1.85
3. Field Of View ± 6.8°
4. Image format (mm) > 16
5. Thickness (Centre of the
Lens) (in mm)* 19.603 19.586 19.437 19.438
6.
Lens Vertex (measured
from center) to Image
Plane Separation (in
mm)*
2.518
± 0.2
2.5015
± 0.2
2.508
± 0.2
2.520
± 0.2
7. Design MTF, 50 lp/mm 0.39 0.43 0.49 0.47
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SAC-ISRO Page 11 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
8. MTF (Realizable, Post
Fabrication)*
(at 50 lp/mm)
0.28 0.32 0.38 0.35
9.
Spectral range
(a) Central wavelength
(nm) 485 555 650 815
(b) Half Power Band
Width (nm) 70 70 60 90
10. Average transmission
(%) (400 – 900 nm) > 50% (at final lens level, all bands)
* Final details to be provided at the time of order placement
Note: All the parameters during and/or after environmental test shall be measured at
a fixed distance from the flange chosen for initial measurement.
MTF measurement shall carried out in sagittal and tangential directions for all field
points as per following table
MTF measurement at various along and across track field angles
Across track
field 6.80 3.4 0 -3.4 -6.8
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SAC-ISRO Page 12 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION V
QUALITY PROVISIONS
5. 1 Quality Assurance Requirements
Quality assurance requirements consist of
Space qualified material selection and qualification.
Ensuring that the optical components withstand a thermal environment from
−20°C to +60°C without affecting the performance when brought to ambient
The process qualification and control.
Qualification and acceptance test requirements.
Contamination control.
Vendor shall carry out qualification testing on witness samples for coating
qualification, described in the successive sub-sections of this document. The
supplier/vendor should provide the reflection and transmission data for reflective & AR
coating on witness samples in the form of EXCEL files after the design is completed,
but before the actual coating starts.
5.1.1 Material
The material used for fabrication of the lens shall be of space/military grade. The
substrate material used for fabrication of the lens shall be free from strain, internal
stresses and internal defects. The material from the same batch shall be used for
fabrication of all the components including witness samples.
Materials, which are nutrients for fungus, shall not be used. Materials used shall be of
low out gassing type with TML
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SAC-ISRO Page 13 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
5.1.3 Surface Quality
The optical surfaces shall have of cosmetic defects such as digs, scratches, pits, pin
holes and sleeks as per MIL-PRF-13830B. The permissible tolerance for scratches and
digs shall be 60-40.
5.1.4 In-process Quality Control Requirements
The manufacturer shall ensure the quality control for realizing a high quality product.
Manufacturer shall provide fabrication flow chart with Key Inspection Points (KIP).
The quality control shall also include, but not limited to, the following process
qualification details of coating, diamond turning etc.
A detailed quality control document shall cover:
- List of proposed materials with outgassing details and material vendors.
- Configuration control.
- Traceability includes batch number, fabrication lot number and component
identification.
- Cleanliness control.
- Process qualification details of coating.
- Non-conformance plan.
Non-conformance at any stage, which affects the quality and reliability of the product,
should be immediately reported to SAC and the required clearance shall be taken from
SAC. This data should be recorded and made available as and when required.
5. 2 Qualification Tests Requirements
Only qualified processes shall be adopted while fabricating the lens. The qualification
test level & test matrix for coating qualification (both Reflective & Anti-reflection)
is given in Table 5.1 & Table-5.2. Minimum size of Witness Samples (WS) would be
1 inch. The methods and procedures for measurement of parameters along with the test
equipment, their calibration and individual parameter limits should be communicated
prior to qualification exercise.
Table 5.1: Test Matrix for qualification of coating on witness samples
Sr. No.
WS 1
WS 2 WS 3 WS 4
1 VI,SR VI,SR VI,SR VI,SR
2 Cold Storage Humidity Thermal Cycle Thermal Shock
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SAC-ISRO Page 14 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
3 Hot Storage VI,SR VI,SR VI,SR
4 VI,SR Abrasion Adhesion -
5 - VI VI -
Table 5.2: Test Levels
Tests For Coating Qualification on
Witness
(AR & Reflective Coating)
For Lens acceptance
Cold Storage Temp: - 20º ± 1º C;
Duration: 24 hrs.
Temp: - 20º ± 1º C;
Duration: 24 hrs.
Hot Storage Temp: 60º ± 1º C;
Duration: 24 hrs.
Temp: 60º ± 1º C;
Duration: 24 hrs.
Humidity R.H. 95%
Temp: + 50º C
Time: 24 hrs
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Thermal Cycling Temp: - 20º to + 60º ± 1º C;
Dwell time: 2hrs ± 5 min
Transition rate: 3°C /min
No. of Cycles :10
Temp: 0º to + 50º ± 1º C;
Dwell time: 2hrs ± 5 min
Transition rate: 3°C /min
No. of Cycles :3
Thermal Shock Temp: - 20º to + 60º ± 1º C;
Dwell time: 5 min
No. of Cycles :200
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Adhesion As per MIL 13830/ MIL-C-675 -
Abrasion As per MIL 13830/ MIL-C-675 -
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SAC-ISRO Page 15 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION VI
TEST REQUIREMENTS Tests shall be conducted to verify the fabrication, workmanship and performance of the
lenses. Proper test setup(s) need to be made (in consultation with SAC) to ensure
measurement accuracies. Fabrication and testing of the lens is the responsibility of
supplier.
The parameters to be measured at component level of lens fabrication/testing are given
below: -
Table 6.1 Performance compliance matrix
S. No Parameter Specification
1. Material properties Procurement
2. Thermal cycling for stress relieving Before coating
3. Radius of curvature / Conic of all surfaces Before coating
4. SAG data Before coating
5. All physical dimensions Before coating
6. Surface quality (Scratch/dig) Before coating
7. Surface roughness Before coating
8. Surface figure Before coating
9. Reflectance & Transmission Witness sample
10. Clear Aperture After coating
The supplier shall submit the methods and procedures of all the tests for measurement
of parameters to meet the specifications. All the results at fabrication level and at post-
fabrication test level shall be provided to SAC in both hard and soft copies. The final
performance parameters with tolerances after achieving the required performance shall
be measured and provided.
6.1. Test Results Properties of the materials (physical, chemical and optical) used for optical component
fabrication and compliance certificates shall be supplied to SAC. The supplier should
provide details of the measurement set-ups as well as the measurement conditions along
with the appropriate data and the digital data in Excel format of the qualified/accepted
component level measurements along with results of witness samples (before and after
each qualification test).
-
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
After fabrication of lens, following environmental tests shall be carried out for acceptance of the lens. Test levels are as per Table-2.
Table 6.2: Test Plan & Test Matrix
SR.
No Test
VI
(Note 1)
All
parameters of
tables 4.1 / 6.1
(Note – 2)
T MTF
(Note 3) COLL Remarks
1 Initial Bench Test at Ambient X X X X X
2 Storage Test
Post Cold
Post Hot
X
X
X
X
X
X
Note – 3
3 Post Thermal Cycling Test /
Final Bench Test at Ambient X X X X X Note – 3
Notes of Table 6.2
Note 1 Visual inspection for holes, digs, bubbles, breakage, deformation, scratches, stresses, peeling of coatings, etc.
Note 2 For testing the parameters of the optics, optical equivalent of detector window, shall be placed near focal plane. The parameters that
shall be measured are EFL, image format, spectral characteristic, transmission, MTF (in 5 planes for each band), collinearity, mechanical
parameters and weight.
Note 3 Parameters of optics shall be measured at ambient conditions.
-
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
ABBREVIATIONS:
VI = Visual Inspection
EFL = Equivalent Focal Length
T = Transmission
MTF = Modulation Transfer Function
COLL = Collinearity
6.2. Rework criteria
If the supplier observes deviations from the specifications at any stage, the rework
criteria required to meet the specification, shall be provided by the supplier with proper
justification and analysis for approval of SAC before proceeding further.
6.3. Shelf life
The lens should meet the performance parameters in the standard lab conditions without
any severe degradation of performance. The manufacturer shall also specify the storage
conditions necessary to ensure the shelf life. Procedures to be adopted for cleaning shall
be specified.
6.4. Acceptance / Rejection Criteria The components shall retain their environmental durability & mechanical integrity and
shall not visually show any sign of chipping, cracking of glass/coating. The acceptance
of final product is based upon its compliance with all the specifications/requirements
laid down in the previous sections.
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SAC-ISRO Page 18 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION VII
DOCUMENTS REQUIRED
7.1 Document details
The documents shall include the following:
Declared material list
Certificates for all the materials
Optical parameters of all the materials used for fabrication
Fabrication plan, particularly addressing the procedure and method of realization including processes to be used for coating annular zones
Detailed test procedure to measure surface quality of the component.
Description of test facilities, environmental conditions and operational details
Failure criteria, test termination criteria etc.
List of equipment, needed for functional test and full performance test and their calibration details.
Procedure to measure Surface Sag on Aspheric Surfaces.
Cleaning procedure for the coated surface of lens.
Storage, cleanliness control, packaging, handling details.
7.2 Non – Conformance Report
This shall contain any non-conformance to the specifications of components and optics.
These are to be immediately reported as soon as they are observed.
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SAC-ISRO Page 19 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
SECTION VIII
DELIVERABLES AND PACKAGING
8.1 Deliverables
Total Deliverables One (1) Origami Lens each for all 4
bands B1 – B4 meeting the RFP
specifications (Total 4 nos. of lenses)
Witness samples Three (03) pieces of 1” diameter with
each coating batch for each type of
coating (AR & Reflective). Total 6 nos.
A single supplier has to provide all the components given in the sections above.
All documents required as per details given in section VII.
8.2 Packaging
The Origami Lens shall be packed carefully in order to protect it from damage during
transit. Each individual package and their intermediate package shall be fixed within
the shipping package which shall be resistant to mechanical shocks, humidity and dust.
Specific care has to be taken to protect the reflective coating on the optics.
The documentation shall be enclosed in the shipping package.
8.3 Delivery Schedule
The schedule for the supply of the origami lens shall be as follows
1. Placement of Purchase Order T0
2. Delivery of coating samples T1 (T0 + 45) days
3. Delivery of Origami lens T1 + 75 days
*To will be date of Order Placement and receipt of order by the vendor
*T1 will be date of go ahead after performance verification from SAC (Typically around 30 -45 days from date of receipt of coating samples / test optics)
8.4 Warranty: One Year Standard Warranty for optics
-
SAC-ISRO Page 20 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
General Instructions
General Instructions, terms and conditions
1.1 Vendor should send the offer in duplicate.
1.2 The offer including discount if any, should be valid for at least 120 days
from the date of opening / due date of the tender.
Vendor should fill up compliance against each of the requirements mentioned in
Annexure 5 and all sections of RFP and submit along with the proposal. Providing
incomplete / no details on any point shall be treated as non-compliance.
-
SAC-ISRO Page 21 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
ANNEXURE – 1
Design / Sag Specifications – Band 1
Zemax Listing
Specifications Details
Entrance Pupil Diameter 65 mm (82.7% Obscured) Temperature 20°C Pressure 1 atm Max. Radial Field ±6.8 degrees Wavelength (Primary) 485 nm
# Comment Type Radius Thickness Glass Diameter Conic Aspheric A4 Aspheric A6 Aspheric A8 Aspheric A10 Aspheric A12
OBJ STANDARD Infinity Infinity 0 0.000 - - - - -
STO STANDARD Infinity 0.0000 65 0.000 - - - - -
2 Input Ap. STANDARD Infinity 20.092 CAF2 65 0.000 - - - - -
3 Zone 1 EVENASPH -106.949 -16.916 MIRROR 67.37318 -1.700 -2.97144805E-07 -5.47394030E-10 8.65130879E-13 -5.85597446E-16 1.46859969E-19
4 Zone 2 EVENASPH -188.419 16.597 MIRROR 47.57645 -3.000 -3.83031949E-06 1.38914520E-09 3.13253348E-13 -5.57617554E-15 2.79196783E-18
5 Zone 3 EVENASPH -488.598 -19.737 MIRROR 49.0809 -3.000 -7.12033951E-06 5.88786820E-09 -8.11287761E-12 7.32946921E-15 -3.02246178E-18
6 Zone 4 EVENASPH -144.493 19.603 MIRROR 23.92666 -3.000 -1.53946195E-05 -1.62017755E-08 -7.77873420E-11 5.88634286E-14 -6.78092625E-16
7 EVENASPH Infinity 0 CAF2 17.99427 0.000 - - - - -
8 Back Working Margin STANDARD Infinity 1.068 17.99427 0.000 - - - - -
9 Detector Window STANDARD Infinity 0.7 D263TECO 17.54539 0.000 - - - - -
10 STANDARD Infinity 0.75 17.35515 0.000 - - - - -
IMA Image STANDARD Infinity 17.07213 0.000 - - - - -
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SAC-ISRO Page 22 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
Design / Sag Specifications – Band 2
Zemax Listing
Specifications Details
Entrance Pupil Diameter 65 mm (82.7% Obscured) Temperature 20°C Pressure 1 atm Max. Radial Field ±6.8 degrees Wavelength (Primary) 555 nm
# Comment Type Radius Thickness Glass Diameter Conic Aspheric A4 Aspheric A6 Aspheric A8 Aspheric A10 Aspheric A12
OBJ STANDARD Infinity Infinity 0 0.000 - - - - -
STO STANDARD Infinity 0.0000 65 0.000 - - - - -
2 Input Ap. STANDARD Infinity 20.100 CAF2 65 0.000 - - - - -
3 Zone 1 EVENASPH -105.496 -16.906 MIRROR 67.37323 -3.000 -4.83019304E-07 -1.69683651E-10 3.19441933E-13 -2.35951972E-16 6.24211069E-20
4 Zone 2 EVENASPH -178.850 16.562 MIRROR 47.57885 3.000 -3.41012616E-06 1.93156262E-09 -3.37121442E-12 7.34248562E-16 -8.60890407E-19
5 Zone 3 EVENASPH -470.297 -19.721 MIRROR 49.06208 3.000 -6.90423944E-06 5.19434669E-09 -6.72838264E-12 5.89868441E-15 -2.44171406E-18
6 Zone 4 EVENASPH -144.816 19.586 MIRROR 23.94057 3.000 -1.50155155E-05 -1.71097673E-08 -7.28694727E-11 8.24723653E-14 -8.33851220E-16
7 EVENASPH Infinity 0.0000 CAF2 17.97689 0.000 - - - - -
8 Back Working Margin STANDARD Infinity 1.0515 17.97689 0.000 - - - - -
9 Detector Window STANDARD Infinity 0.70 D263TECO 17.53278 0.000 - - - - -
10 STANDARD Infinity 0.75 17.34110 0.000 - - - - -
IMA Image STANDARD Infinity 17.05717 0.000 - - - - -
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SAC-ISRO Page 23 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
Design / Sag Specifications – Band 3
Zemax Listing
Specifications Details
Entrance Pupil Diameter 65 mm (82.7% Obscured) Temperature 20°C Pressure 1 atm Max. Radial Field ±6.8 degrees Wavelength (Primary) 650 nm
# Comment Type Radius Thickness Glass Diameter Conic Aspheric A4 Aspheric A6 Aspheric A8 Aspheric A10 Aspheric A12
OBJ STANDARD Infinity Infinity 0 0.000 - - - - -
STO STANDARD Infinity 0.0000 65 0.000 - - - - -
2 Input Ap. STANDARD Infinity 19.9880 CAF2 65 0.000 - - - - -
3 Zone 1 EVENASPH -104.216 -16.8000 MIRROR 67.35033 -1.541 -3.6115486E-07 3.2111650E-11 -1.4831400E-14 -1.9620443E-17 1.0132446E-20
4 Zone 2 EVENASPH -177.133 16.4120 MIRROR 47.58102 -3.000 -3.3650547E-06 2.1483623E-09 -5.6608943E-12 4.8844096E-15 -3.4243168E-18
5 Zone 3 EVENASPH -507.495 -19.5610 MIRROR 49.0073 -3.000 -7.0379895E-06 5.0675951E-09 -6.2237348E-12 5.2897667E-15 -2.1953376E-18
6 Zone 4 EVENASPH -143.988 19.4370 MIRROR 23.84556 -3.000 -1.5597410E-05 -1.7923980E-08 -7.9962735E-11 1.4400435E-13 -1.1297964E-15
7 EVENASPH Infinity 0.0000 CAF2 17.93379 0.000 - - - - -
8 Back Working Margin STANDARD Infinity 1.0577 17.93379 0.000 - - - - -
9 Detector Window STANDARD Infinity 0.7000 D263TECO 17.48833 0.000 - - - - -
10 STANDARD Infinity 0.7500 17.29672 0.000 - - - - -
IMA Image STANDARD Infinity 17.01984 0.000 - - - - -
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SAC-ISRO Page 24 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
Design / Sag Specifications – Band 4
Zemax Listing
Specifications Details
Entrance Pupil Diameter 65 mm (82.7% Obscured) Temperature 20°C Pressure 1 atm Max. Radial Field ±6.8 degrees Wavelength (Primary) 815 nm
# Comment Type Radius Thickness Glass Diameter Conic Aspheric A4 Aspheric A6 Aspheric A8 Aspheric A10 Aspheric A12
OBJ STANDARD Infinity Infinity 0 0.000 - - - - -
STO STANDARD Infinity 0.0000 65 0.000 - - - - -
2 Input Ap. STANDARD Infinity 20.007 CAF2 65 0.000 - - - - -
3 Zone 1 EVENASPH -103.037 -16.794 MIRROR 67.35326 -2.081 -4.50506085E-07 3.00676919E-10 -4.16826892E-13 2.39815413E-16 -5.27216109E-20
4 Zone 2 EVENASPH -168.716 16.390 MIRROR 47.59015 -3.000 -3.10531082E-06 2.46202305E-09 -8.16807563E-12 9.23671280E-15 -5.90787755E-18
5 Zone 3 EVENASPH -479.046 -19.565 MIRROR 48.99738 -3.000 -6.78405751E-06 4.33932931E-09 -4.80800451E-12 3.80965161E-15 -1.56830178E-18
6 Zone 4 EVENASPH -144.473 19.438 MIRROR 23.89769 -3.000 -1.53010311E-05 -2.00607716E-08 -5.49579215E-11 3.79921612E-14 -9.22805545E-16
7 EVENASPH Infinity 0.0000 CAF2 17.95362 0.000 - - - - -
8 Back Working Margin STANDARD Infinity 1.0703 17.95362 0.000 - - - - -
9 Detector Window STANDARD Infinity 0.70 D263TECO 17.50104 0.000 - - - - -
10 STANDARD Infinity 0.75 17.30809 0.000 - - - - -
IMA Image STANDARD Infinity 17.01944 0.000 - - - - -
The final design specifications for all bands shall be provided at the time of order placement.
-
SAC-ISRO Page 25 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
ANNEXURE – 2
COATING / BLACK PAINT ON LENS: SPECIFICATIONS
Front Surface:
The specifications are given below for the front surface:
Figure A.1: Schematic showing the metal-coating and black-paint details for front
surface of the multi-fold lens
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SAC-ISRO Page 26 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band-1: Front*
Figure A.2: Coating Details
Table A.1: Specifications for Coating and Black-paint for the front
surface of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 12.4 Coated Region
2. 12.4 15.3 Black-Painted Region
3. 15.3 24.3 Coated Region
4. 24.3 26.85 Black-Painted Region
5. 26.85 32.5 Input Aperture (Anti
reflection coated)
6. 32.5 35 Black-Painted Region * Final details shall be provided at the time of order placement
35 mm 32.5 mm
26.85 mm
24.3 mm
15.3 mm
12.4 mm
-
SAC-ISRO Page 27 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band-2: Front*
Figure A.3: Coating Details
Table A.2: Specifications for Coating and Black-paint for the front
surface of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 12.45 Coated Region
2. 12.45 15.2 Black-Painted Region
3. 15.2 24.3 Coated Region
4. 24.3 26.85 Black-Painted Region
5. 26.85 32.5 Input Aperture (Anti
reflection coated)
6. 32.5 35 Black-Painted Region * Final details shall be provided at the time of order placement
35 mm 32.5 mm
26.85 mm
24.3 mm
15.2 mm
12.45 mm
-
SAC-ISRO Page 28 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band-3: Front*
Figure A.4: Coating Details
Table A.3: Specifications for Coating and Black-paint for the front
surface of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 12.4 Coated Region
2. 12.4 15.2 Black-Painted Region
3. 15.2 24.3 Coated Region
4. 24.3 26.85 Black-Painted Region
5. 26.85 32.5 Input Aperture (Anti
reflection coated)
6. 32.5 35 Black-Painted Region * Final details shall be provided at the time of order placement
35 mm 32.5 mm
26.85 mm
24.3 mm
15.2 mm
12.4 mm
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SAC-ISRO Page 29 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band-4: Front*
Figure A.5: Coating Details
Table A.4: Specifications for Coating and Black-paint for the front
surface of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 12.55 Coated Region
2. 12.55 15.2 Black-Painted Region
3. 15.2 24.3 Coated Region
4. 24.3 26.85 Black-Painted Region
5. 26.85 32.5 Input Aperture (Anti
reflection coated)
6. 32.5 35 Black-Painted Region * Final details shall be provided at the time of order placement
35 mm 32.5 mm
26.85 mm
24.3 mm
15.2 mm
12.55 mm
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SAC-ISRO Page 30 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Rear Surface:
The specifications for the rear surface are given below:
Figure A.6: Coating details for the rear surface
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SAC-ISRO Page 31 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band - 1: Rear*
Figure A.7: Coating details for the rear surface
Table A.5: Specifications for Coating and Black-Paint for the rear surface
of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 9.4 Anti reflection coated
region (Output from
Lens)
2. 9.4 24.85 Coated Region
3. 24.85 25.35 Black Painted region
4. 25.35 34 Coated Region
5. 34 35 Black Painted Region * Final details shall be provided at the time of order placement
35 mm 34 mm
25.35 mm 24.85 mm
9.4 mm
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SAC-ISRO Page 32 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band - 2: Rear*
Figure A.8: Coating details for the rear surface
Table A.6: Specifications for Coating and Black-Paint for the rear surface
of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 9.4 Anti reflection coated
region (Output from
Lens)
2. 9.4 25 Coated Region
3. 25 25.3 Black Painted region
4. 25.3 34 Coated Region
5. 34 35 Black Painted Region * Final details shall be provided at the time of order placement
35 mm 34 mm
25.3 mm 25.0 mm
9.4 mm
-
SAC-ISRO Page 33 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band - 3: Rear*
Figure A.9: Coating details for the rear surface
Table A.7: Specifications for Coating and Black-Paint for the rear surface
of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 9.4 Anti reflection coated
region (Output from
Lens)
2. 9.4 24.8 Coated Region
3. 24.8 25.4 Black Painted region
4. 25.4 34 Coated Region
5. 34 35 Black Painted Region * Final details shall be provided at the time of order placement
35 mm 34 mm
25.4 mm 24.8 mm
9.4 mm
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SAC-ISRO Page 34 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Specifications for Band - 4: Rear*
Figure A.10: Coating details for the rear surface
Table A.8: Specifications for Coating and Black-Paint for the rear surface
of the lens
S.No. Start (Radial,
mm)
End (Radial,
mm)
Specifications
1. 0 9.4 Anti reflection coated
region (Output from
Lens)
2. 9.4 24.9 Coated Region
3. 24.9 25.3 Black Painted region
4. 25.3 34 Coated Region
5. 34 35 Black Painted Region * Final details shall be provided at the time of order placement
35 mm 34 mm
25.3 mm 24.9 mm
9.4 mm
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SAC-ISRO Page 35 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
ANNEXURE – 3
TOLERANCE SPECIFICATIONS
FRONT AND REAR SURFACE:
S.NO. Parameter Specification
1. Thickness ± 5µm
2. Radius of Curvature (Zones) ± 0.02 %
3. Decenter (Zones) ± 2 µm
4. Decenter (Rear w.r.t. Front Surface) ± 2 µm
5. Tilt (Zones) ± 0.2 arc-min
6. Tilt (Rear w.r.t. Front Surface) ± 0.5 arc-min
7. Irregularity 0.5 fringe (→632 nm)
8. Homogeneity (Glass) Better than 1 x 10-5
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SAC-ISRO Page 36 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
ANNEXURE – 4
References
1. ‘Ultrathin cameras using annular folded optics’, Eric and Tremblay, Applied
Optics, Volume 46, No. 4, pp. 463-471
2. ‘Relaxing the alignment and fabrication tolerances of thin annular folded
imaging systems using wavefront coding’, Eric and Tremblay, Applied Optics,
Volume 46, No. 27, pp. 6751-6758
3. ‘Ultrathin four-reflection imager’, Eric and Tremblay, Applied Optics, Volume
48, No. 2, pp. 343-354
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SAC-ISRO Page 37 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
ANNEXURE – 5
Compliance matrix for RFP (To be filled by vendor with necessary remarks as applicable)
Section Details Compliance by
vendor with remarks
1 Introduction
1.1 Scope
1.2 General description of Origami Lenses
1.3 Applicable documents
1.4 Test Sequence
1.5 Conditions and methods of tests
1.6 Supplier responsibility
1.7 Inspection rights
2.1 Optical / mechanical / thermal requirements
2.2 Scope of Work
2.3 Sequence of Activities
2.4 AR Coating
2.5 Metallic reflective coating
2.6 Black Painting
3 Specifications of front and rear surfaces
3.1 Table 3.1 – Specifications of 4-fold Origami lens
4 Final Specifications of Origami Lens
4.1 Table 4.1 – Specifications – Lens performance
parameters
5 Quality provisions
5.1 Quality Assurance Requirements
5.2 Qualification tests requirements
6 Test Requirements
6.1 Test results
6.2 Rework criteria
6.3 Shelf life
6.4 Acceptance/ Rejection criteria
7.1 Documents required
7.2 Non-conformance report
8.1 Deliverables
8.2 Packaging
8.3 Delivery Schedule
8.4 Warranty
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SAC-ISRO Page 38 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
Table 3.1 – Specifications of Origami lens
S.No. PARAMETER SPECIFICATION Compliance with
remarks
1. Material CaF2
2. Surface As per the Surface Sag
specifications / ZEMAX®
design given in Annexure -1 for
all 4 bands B1 – B4
3. Shape of the Lens Circular
4. Physical Diameter Between 70.00mm and 75.00
mm
5. Clear Aperture 65.00mm (Refer Annexure 1
and 2 for details)
6. Surface Profile Aspheric (Both at front and rear)
(Refer Annexure 1 and 2 for
details)
7. Circularity at Edges
Mounting Surface Finish
Within 1 micron
Shall be finished to Emery 303
(or equivalent)
8. Chamfering Sharp edges of the lens shall be
chamfered to around 0.5mm
9. Surface Figure (Over the
Full Active Area) Better than /6 Peak-to-Valley
/35 RMS, → 632.8 nm (He-
Ne)
10. Scratch/Dig 60/40 or better
11. Surface Roughness Less than 5 nm
12. Reflectance
At all Angles of Incidence
Enhanced Al Coating /
Silver Coating (mutually
agreed upon) with an
additional Protective
Overcoat over the entire
active area
Average ≥ 88%
(0.4 – 0.9 microns)
Measurement of reflectance to
be carried out through CaF2
glass with 5 mm thickness of
material.
(refer section 2.5)
13. Coating Pinholes There should be no pinholes
visible in the coating when it is
illuminated by a bright source of
light / backlit (As per relevant
MIL standard)
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SAC-ISRO Page 39 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
14. Coated Area Please refer Annexure 2
15. Tolerance on Coated Area
(For S.No.14.)
±50 microns
16. Coating Thickness
Uniformity
Better than 1 percent (desirable)
17. Uncoated Area (Annular
Aperture for Light Input,
Rear Central Portion for
Light Exit)
Please refer Annexure 2
18. Black Painted Area
Qualified black paint shall be
used. Please refer Annexure 1
19. Anti-Reflection Coating Anti-reflection coating on
uncoated area with less than
0.4% reflection over spectral
range 0.35 – 1.1 microns.
(Please refer Annexure 2 and
section 2.4)
TABLE 4.1
SPECIFICATIONS FOR THE ORIGAMI LENS: LENS
PERFORMANCE PARAMETERS
S.No. PARAMETER SPECIFICATION Compliance
with remarks
B1 B2 B3 B4
1. Effective Focal
Length 67.5 mm ± 1 mm
2. F/Number (Effective) 1.85
3. Field Of View ± 6.8°
4. Image format (mm) > 16 mm
5. Thickness (Centre of
the Lens) (in mm)* 19.603 19.586 19.437 19.438
6.
Lens Vertex
(measured from
center) to Image
Plane Separation (in
mm)*
2.518
± 0.2
2.5015
± 0.2
2.508 ±
0.2
2.520 ±
0.2
7. Design MTF, 50
lp/mm 0.39 0.43 0.49 0.47
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SAC-ISRO Page 40 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other
purpose except for preparation of the offer for fabrication.
8. MTF (Realizable,
Post Fabrication)*
(at 50 lp/mm)
0.28 0.32 0.38 0.35
9. Spectral range
(c) Central
wavelength (nm) 485 555 650 815
(d) Half Power Band
Width (nm) 70 70 60 90
10. Average transmission
(%) (400 – 900 nm) > 50%
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SAC-ISRO Page 41 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
ANNEXURE – 6
Mechanical Drawings
(Final details to be provided at time of order placement)
-
SAC-ISRO Page 42 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
-
SAC-ISRO Page 43 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
-
SAC-ISRO Page 44 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.
-
SAC-ISRO Page 45 of 45
Specifications for fabrication and testing of Origami Lens
The optical design of the multi-fold lenses presented in this RFP is the proprietary work of Space Applications Center (ISRO) and shall not be used for any other purpose except for preparation of the offer for fabrication.