reorientation & lapan tubsat-1 separation

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REORIENTATION & LAPAN TUBSAT-1 SEPARATION REORIENTATION & SEPARATION OF DLA-U WITH PEHUENSAT-1 REORIENTATION & SRE SEPARATION CARTOSAT-2 SEPARATION LAPAN- TUBSAT SEPARATION SATELLITE SEPARATION SEQUENCE SATELLITE SEPARATION SEQUENCE PSLV- C7 CARTOSAT-2 / SRE MISSION PSLV- C7 CARTOSAT-2 / SRE MISSION

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PSLV- C7 CARTOSAT-2 / SRE MISSION. PSLV- C7 CARTOSAT-2 / SRE MISSION. SATELLITE SEPARATION SEQUENCE. REORIENTATION & SEPARATION OF DLA-U WITH PEHUENSAT-1. LAPAN- TUBSAT SEPARATION. REORIENTATION & LAPAN TUBSAT-1 SEPARATION. REORIENTATION & SRE SEPARATION. CARTOSAT-2 SEPARATION. - PowerPoint PPT Presentation

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Page 1: REORIENTATION &  LAPAN TUBSAT-1  SEPARATION

REORIENTATION &

LAPAN TUBSAT-1 SEPARATION

REORIENTATION &

SEPARATION OF DLA-U WITH PEHUENSAT-1

REORIENTATION &

SRE SEPARATION

CARTOSAT-2 SEPARATION

LAPAN- TUBSAT SEPARATION

SATELLITE SEPARATION SEQUENCESATELLITE SEPARATION SEQUENCE

PSLV- C7 CARTOSAT-2 / SRE MISSIONPSLV- C7 CARTOSAT-2 / SRE MISSION

Page 2: REORIENTATION &  LAPAN TUBSAT-1  SEPARATION

Micro gravity Exp.

Change over to eliptical orbit

* 3 axis stabilisation * Sun pointing

* SRE launch in PSLV

SRE Injection

CARTO 2 Injection

Acquisition & orbit determination

Launch phase Orbit phase

SRE first burn (Change to daily repeating elliptical orbit)

Coast phase attitude manoeuveringDeorbit

Recovery

Floatation system UHF Beacon

Parachute deployment

Reentry

Atmospheric braking

elliptical orbit (REO)

Deboost & atmospheric phase

Daily repeating

SSPO

( 20 min.)

SRE – MISSION PROFILE

• SRE will be in orbit for nearly 10 days during which it will perform Micro- Gravity experiments

• Subsequently it will be moved from Circular orbit to Repeating Elliptical Orbit (REO)

• It will de-boosted from REO and will be made to Re-enter and impact nearly 140 km off the coast of SHAR

• SRE will be recovered from the Sea

T0 + 35 minVelocity: 8000 m/s

T0 + 44 minVelocity: 47 m/s

T0 + 46 minVelocity: 12 m/s

20th Jan

Deboost

22nd Jan

Velocity: 7350 m/s

T0

PSLV- C7 CARTOSAT-2 / SRE MISSIONPSLV- C7 CARTOSAT-2 / SRE MISSION

10th Jan

Page 3: REORIENTATION &  LAPAN TUBSAT-1  SEPARATION

Typical visibility: Prior & Post De-boost

Saskatoon, Svalbard, Lucknow, Air- Borne Telemetry (ABT),

Ship Borne Telemetry (SBT), SHAR

PSLV- C7 CARTOSAT-2 / SRE MISSION

De- Boost STARTAltitude : 638 kmLatitude : 4 degLongitude : - 92 deg

De- Boost ENDAltitude : 635 kmLatitude : 52 degLongitude : - 105 deg

RE- ENTRYAltitude : 100 kmLatitude : 27 degLongitude : 84 deg

Data down load regions

Page 4: REORIENTATION &  LAPAN TUBSAT-1  SEPARATION

SHAR

CHENNAI

140 km

50x15 km – Stay out zone for ship

Air borne Telemetry from SHAR

Ship borne Telemetry

Dornier aircraft from Chennai

Chetak Helicopter from Sarang

ICG Ship - Sarang

DEPLOYMENT OF RECOVERY SYSTEMS

Probable impact zone 30x5 km

Reentry ground trace

50 km

15 km

PSLV- C7 CARTOSAT-2 / SRE MISSION

Page 5: REORIENTATION &  LAPAN TUBSAT-1  SEPARATION

EDUSATEDUSAT