STPSat 2 [Ball]
STPSat 3 [Ball]
STPSat 2 is an experimental spacecraft for STP (Space Test Program). It was the first flight of the Standard Interface Vehicle (STP-SIV).
STPSat-2 carried three experimental payloads that were chosen by the DoD Space Experiment Review Board:
STPSat 3 is a copy of the STPSat-2 satellite, which carried five experiments, including a module designed to host various space situational awareness sensors and a pair of space environment sensors.
In addition, the spacecraft has new capability, the MMA Design LLC De-Orbit Module used to de-orbit the satellite in less than 25 years.
Nation: | USA |
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Type / Application: | Technology |
Operator: | US Air Force (USAF) STP (Space Test Program) |
Contractors: | Ball Aerospace (prime); AeroAstro (bus) |
Equipment: | 2 SPEX, ODTML (#2); iMESA-R, J-CORE, SSU, SWATS, TCTE, De-Orbit Module (#3) |
Configuration: | Astro-200 |
Propulsion: | |
Power: | 3 deployable solar arrays, batteries |
Lifetime: | 1 year |
Mass: | 180 kg |
Orbit: | 641 km × 652 km, 72° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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STPSat 2 (USA 217) | 2010-062A | 20.11.2010 | Kd LP-1 | Minotaur-4 HAPS | with FASTRAC 1, FASTRAC 2, FalconSat 5, FASTSat-HSV 01, RAX 1, O/OREOS, NanoSail-D2, Ballast A, Ballast B | |
STPSat 3 | 2013-064A | 20.11.2013 | WI LA-0B | Minotaur-1 | with ORS 3, ORSES, ORS Tech 1, ORS Tech 2, SENSE 1, SENSE 2, Ho`oponopono 2, Firefly, STARE B, Prometheus 1.1, ..., 1.8, Black Knight 1, NPS-SCAT, COPPER, ChargerSat 1, TJ3Sat, Trailblazer 1, Vermont Lunar Cubesat, SwampSat, CAPE 2, DragonSat 1, KySat 2, PhoneSat v2.4 |
Further STP missions:
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