reorientation & lapan tubsat-1 separation

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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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  • REORIENTATION & LAPAN TUBSAT-1 SEPARATIONREORIENTATION & SEPARATION OF DLA-U WITH PEHUENSAT-1REORIENTATION & SRE SEPARATIONCARTOSAT-2 SEPARATIONLAPAN- TUBSAT SEPARATIONSATELLITE SEPARATION SEQUENCEPSLV- C7 CARTOSAT-2 / SRE MISSIONPSLV- C7 CARTOSAT-2 / SRE MISSION

  • SRE MISSION PROFILESRE will be in orbit for nearly 10 days during which it will perform Micro- Gravity experimentsSubsequently 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 SHARSRE will be recovered from the SeaT0 + 35 minVelocity: 8000 m/sT0 + 44 minVelocity: 47 m/sT0 + 46 minVelocity: 12 m/s20th JanDeboost22nd JanVelocity: 7350 m/s T0PSLV- C7 CARTOSAT-2 / SRE MISSIONPSLV- C7 CARTOSAT-2 / SRE MISSION10th Jan

  • Typical visibility: Prior & Post De-boostSaskatoon, Svalbard, Lucknow, Air- Borne Telemetry (ABT),Ship Borne Telemetry (SBT), SHARPSLV- C7 CARTOSAT-2 / SRE MISSIONDe- Boost STARTAltitude : 638 kmLatitude : 4 degLongitude : - 92 degDe- Boost ENDAltitude : 635 kmLatitude : 52 degLongitude : - 105 degRE- ENTRYAltitude : 100 kmLatitude : 27 degLongitude : 84 degData down load regions

  • SHARCHENNAI140 km 50x15 km Stay out zone for shipAir borne Telemetry from SHARShip borne TelemetryDornier aircraft from ChennaiChetak Helicopter from SarangICG Ship - SarangDEPLOYMENT OF RECOVERY SYSTEMSProbable impact zone 30x5 km Reentry ground trace 50 km15 kmPSLV- C7 CARTOSAT-2 / SRE MISSION

  • EDUSAT