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Company Presentation ISIS Innovative Solutions In Space BV Abe Bonnema Space Economy in the Multipolar World 1 st International Conference, Vilnius, Lithuania, 6-8 October, 2010

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Page 1: Company Presentation ISIS Innovative Solutions In …space-lt.eu › failai › Prezentacijos › Abe Bonnema_Developing...Company Presentation ISIS –Innovative Solutions In Space

Company Presentation

ISIS – Innovative Solutions In Space BV

Abe Bonnema

Space Economy in the Multipolar World

1st International Conference, Vilnius, Lithuania, 6-8 October, 2010

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• Company overview

– ISIS

– CubeSatShop.com

– ISL Launch Services

– IDS Applications

• CubeSat and Nanosats introduction

• Challenges & Opportunities for CubeSats

• Conclusions

Outline

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Why start a space company?

"The way to make a small fortune in

space is to start with a big fortune.

Space is a good place to lose a lot

of money real fast."

John Pike

American Federation of Scientists

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Company Overview

• Spin-off of Delfi-C3 nanosatellite project of TU Delft

• Founded January 06, 2006

• Office locations:

– Delft, near Delft University of Technology Campus

– Noordwijk, in the European Space Incubator at ESTEC

• Current employment: 25+ engineers

• Fully owned by the management team:

Abe Bonnema

Marketing Director

Eddie van Breukelen

Financial Director

Jeroen Rotteveel

Managing Director

Wouter Jan Ubbels

Technical Director

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Company Structure

• Separate „business units‟ for:

– Missions, Platforms, Custom systems

– Off-the-shelf systems from CubeSat system developers

– Small Satellite Launch Services

– Nanosatellite Applications

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Missions and Systems

• Subsystem R&D:

– Disruptive subsystems

– Custom developments

• CubeSat and Nanosat Missions:

– Definition, Design and Development

– Assembly, Integration, Verification

• Ground Stations (Kits) & Mission Operations

• Training and Knowledge Transfer:

– Laboratory Training Kits

– Tailored Space Systems Engineering courses

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Current Activities

• Ongoing Product Developments:

– Communication Systems (UHF, VHF, S-Band)

– ISIPOD Deployer systems in various form factors (e.g. 6-Pack)

– Test & Ground Support Equipment Kits

• Ongoing CubeSat R&D Projects:

– Track & Trace payloads (with Dutch partners)

– Miniaturized Star trackers (with TNO)

– Deployable Solar Arrays (with Dutch Space)

– Cool Gas microPropulsion Module (with TNO / Bradford)

– Modular Payload Deck Elements (with Stork/Fokker/Mecon)

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Current Activities

• Ongoing Missions & Platforms:

– Triton-1 Tech Demo Mission (with SystematIC / NLR)

– Triton-2 AIS Demo Mission (with ClydeSpace / GomSpace)

– FUNcube Platform and MAIV (for AMSAT UK)

– De-Orbit Sail Demo Mission (EU project with SSC, DLR,

ASTRIUM, Universities in Greece, Turkey, South Africa)

– Delfi-n3Xt (Payload Partner of TU Delft)

– 2U environmental monitoring mission (undisclosed customer)

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QB50

“An international network of 50 double CubeSats for multi-

point, in-situ, long-duration measurements in the lower

thermosphere and for re-entry research.”

von Karman Institute

for Fluid Dynamics

• Consortium led by VKI – Von Karman Institute (J. Muylaert)

• Supported by space agencies

• ISIS involved for:

– Satellite Platform Technical Advice

– Launch Configuration and Orbit Dynamics Analysis

– Payload Deck, Deployment System and Integration Support

– Launch Campaign Support

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International Project Support

• HumSat

– UN supported humanitarian mission

– Satellite constellation to receive low data rate

terrestrial sensor data

– Receiver technology key to success

– Ground Station network required

• GENSO

– GENSO compatible Ground Stations

– GENSO validation mission support

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Advanced Application - OLFAR

• OLFAR is a new concept of a low frequency radio telescope in

space using small satellites.

• Correlation must be done in space.

• Distributed processing with centralized downlink transmission is

the preferable option.

• Inter satellite link is the communication challenge.

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Company Structure

• Separate „business units‟ for:

– Missions, Platforms, Custom systems

– Off-the-shelf systems from CubeSat system developers

– Small Satellite Launch Services

– Nanosatellite Applications

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CubeSatShop.com

• Objectives:

– One-stop-shop for all your off-the-shelf CubeSat systems

– Single portal for questions and system comparison

– CubeSat configurator interface

• Current Partners (new partner/products always welcome)

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Company Structure

• Separate „business units‟ for:

– Missions, Platforms, Custom systems

– Off-the-shelf systems from CubeSat system developers

– Small Satellite Launch Services

– Nanosatellite Applications

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Last month: 1 year in orbit – Congrats to:

• ISILaunch01 teams:

UWE-2 BEESAT ITUpSAT1 SwissCube

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Company Structure

• Separate „business units‟ for:

– Missions, Platforms, Custom systems

– Off-the-shelf systems from CubeSat system developers

– Small Satellite Launch Services

– Nanosatellite Applications

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Introduction to CubeSats | Nanosats

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CubeSats | Nanosats

• Classed by size (mass):

– Picosatellite

• Up to 1 kg

• CubeSat standard

– Nanosatellite

• Up to 10 (or 25 ?) kg

• CubeSat standard

– Microsatellite

• Up to 100 - 200 kg

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• Characterized by:

– Typical mission objectives

– Development time

– Developer‟s background and

experience

– Design and test philosophy

– Launch and orbit requirements

CubeSats | Nanosats

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• Development time:

– Relatively short; 1-3 years „from scratch to space‟

– Extreme case, responsive space; possibly 3 months

– Independent of small satellite class

• Developer‟s background and experience:

– Increased accessibility allows new developers to space

– From hobbyist group to established space industry

– Varying experience – satellite development / launch

CubeSats | Nanosats

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• Design and test philosophy:

– Limited resources often a driver for design choices

– Components:

• COTS vs. space qualified

– Model philosophy:

• proto-flight vs. EM/QM/FM

– Documentation:

• time vs. traceability

– Testing:

• minimal vs. full qualification/acceptance

CubeSats | Nanosats

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• Launch and orbit requirements:

– Depend on mission objectives, but often quite „relaxed‟

– Orbital altitude requirements, range vs. specific:• e.g. between 500-1000 km

– Inclination often driven by developer‟s location:• Operations from developer‟s local ground station

• Sun Synchronous in many cases preferred

– Timing and schedule driven by various parameters:• Objected satellite readiness

• Political/budgetary aspects

– Search for launch at T - 6 to 18 months…

CubeSats | Nanosats

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Why build CubeSats | Nanosats?

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Disruptive technology

Mainframe Mini-Computer PC

Large Spacecraft Microsatellite Nanosatellite

Disruptive Technology

-Improve a product or service in a way the market does not expect

- Often at low performance but at significantly lower price

- Often targeted at customers with different needs

- Has the ability to radically change the entire market

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Disruptive Technology

1st generation Cubesats

Rad-Tolerant Cubes

Highly capable SC

Start simple- Low pointing

- Low complexity

- Fast time to market

Stepwise

Improvements~3 year lifecycles

-Formation Flying

-Better Pointing

-Lifetime (rad hard)

-Reliability

Design to Cost-Focused Missions

-New risk approach

-Low entry barrier

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CubeSat Pointing Trends

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Design Aspects

• Small Teams

• Short Mission Lifecycles

• Modular systems

• Standard avionics modules and interfaces

• Mission Specific Avionics and systems

• Plug and Play Payload capability

• Off-the-shelf systems

1 kg, 1W 15 kg, 40W

Part commonality

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Lowering entry barriers

• Traditionally:

– Big Agencies fly „higher risk‟ missions with new technologies

– Once proven, the technology flows to commercial (e.g. GEO SATCOM) missions

• With CubeSats | Nanosats:

– Small research groups can take on missions due to lower mission cost and prepare the organization and workforce for larger missions

– Entrepreneuring companies can fly „risky‟ technology on commercial missions due to lower financial risk

– Lower infrastructure cost and more access to space enables affordable constellations

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CubeSat | Nanosat Applications

• Educational:

– training of new engineers

• Technology and component validation:

– demonstrating propulsion systems, sensors

• Scientific:

– microgravity, astronomy, space weather

• Institutional / Operational/ Military:

– Earth observation

– Monitoring and surveillance

– signal intelligence,

– communications

• Commercial:

– monitoring of ships, dikes, containers

• PR and Private initiatives:

– Commercials

– Luxury items

Turn key

Solutions

Support,

Capacity

Building

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CubeSat | Nanosats

• Mission objectives:– Education - gain experience

– Demonstration - add functionality

– Scientific - increase performance

– Operational/Commercial - increase reliability

• The Challenges = the Opportunities:

– Frequencies and legislation

– Cooperation

– Access to space

– Standardization

– Increase functionality, performance and reliability

– Overcome technical bottlenecks

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• Frequencies and downlink of data, operations:

– Amateur frequencies

• Need for improved coordination?

• Re-use / sharing of frequencies?

– Networks of CubeSats

• How do you coordinate 25+ Cubes deployed at the same time (e.g. QB50)?

• Scheduling (TDMA)?

– Shared ground stations

• Licensing & regulatory aspects?

• Training of operation?

• Data policies?

Challenges & Opportunities

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• Improved Cooperation

– Develop your strengths, do not re-invent the wheel

– Regulatory issues and restrictions

• E.g. ITAR vs non-dependence movement in Europe

• Licensing

– IPR issues in cooperation between parties

• Industry / Industry: competitors vs. partners

• Industry / Academia: risk your IPR to become public domain

• Academia / Industry: risk of not being allowed to publish your work

• Industry / government: risk w.r.t. IPR ownership

Challenges & Opportunities

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• Improve access to space

– Launches are not cheap

• Launch fees

• Testing and procedures

• Campaign cost

– More often regulations apply

(e.g. national space laws, NOAA, ITU/FCC)

– Do not underestimate the level of testing and prove

of conformance required by the LSP

– Take into account end-of-life

Challenges & Opportunities

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• Standardization and modularity

– CubeSat Standard, universally adopted?

• Depends very much on the type of deployer used for

things like envelope, mass, etc

• Variations on CubeSats are not very well covered

• Mostly covers form, fit, mechanical aspects

– Standardization of internal interfaces:

• No real solution or consensus (mech, data, power, etc)

• If you say: “we use our own standard”, it‟s not a

standard.

• Commercial CubeSat systems providers struggle with

this quite a bit…

Challenges & Opportunities

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Challenges & Opportunities

• Technical bottlenecks:

– Envelopes: volume, mass

– Miniaturization of systems

– Budgets (and not just financial):

Control

Power

Communication

Link Margin

Data rates

Orbit average power

Battery sizing

Stabilization

Pointing Accuracy

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Goals:

• Better efficiencies

• Higher data rates

• Reliable links

Communication

Closing the link:

UHF/VHF Transceivers

S-band Transmitter

Deployable Antenna Systems (VHF/UHF)

Ground Stations

Challenges & Opportunities

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Goals:

• Better efficiencies

• Increased Orbit Average Power

• Longer (battery) lifetime

EPS -> flexibility

Batteries -> higher capacity

Increased Power:

Modular Deployable Solar Panels

(up to 2x3 panels, or 42 cells/3U)

Power

Challenges & Opportunities

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Goals:

• 3-Axis attitude control

• Accurate determination

• Enable Formation Flying / Swarms

Some examples:

Control

• Miniature Fine Sun Sensors

• Multi-Aperture Star Trackers

• „Facet Nano‟ for Cubesats

• Micropropulsion

Challenges & Opportunities

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• Develop more capable subsystems:

– Attitude control systems and sensors

– Propulsion and orbit control systems

– More efficient power systems

– Power generation and storage

– Higher data rate communication

– More efficient communication systems

– …

• Focus on applications:

– Which (information) needs that can be fulfilled with such small platforms?

– What scientific questions may be answered with small satellite missions?

– What other applications can you think of?

Opportunities enough…

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Conclusions

• CubeSats and Nanosats:

– Low cost, low barrier access to space

– Perfect training platforms for technology and knowledge building

– Affordable missions from demonstration to scientific,

commercial and operational

– First step in a roadmap to more capable platforms

• Opportunities for Baltic region:

– Cooperative CubeSat mission for knowledge building

– Determine what niche and applications to focus on

– Become a big player in small space

“The biggest limitation in (very) small satellites is your creativity…”

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ISIS - Innovative Solutions In Space BV

Thank you for your attention!

Abe Bonnema

Marketing Director

Molengraaffsingel 12-14

2629 JD Delft, The Netherlands

e-mail: [email protected]

web: www.isispace.nl | www.isilaunch.com

www.cubesatshop.com | www.innovativedataservices.com