2008-F01
SpaceDev (Poway, Calif.) MMB-100 Trailblazer developed for the US MDA DSE (Distributed Sensing Experiment) and then cancelled; bus to be launched with no payload as a test payload for Falcon 1 as part of DoD Operationally Responsive Space (ORS) program.
Mass is 83.5 kg.
Launch with Nanosail-D PPOD and PreSat PPOD. The SPASS Secondary Payload Adaptor and Separation System was developed by the Malaysian company ATSB and Space Access Technologies of Ashburn, VA.
Planned orbit is 330 x 685 km x 9 deg. Total payload 170 kg. Falcon 1 uses an improved Merlin 1C engine.
| F1-3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2008 Aug 3 | 0334 | Launch by Falcon 1 | KMR Omelek |
| 0336 | T+2:10 Inertial guidance, 35 km, 1.050km/s | ||
| 0336 | T+2:20? Vehicle anomaly | ||
| 0336 | T+2:43 Stage 2 burn | ||
| 0336 | Stage 1 recontact stage 2 | ||
| T+3:13? Fairing sep | |||
| Apogee 217 km | |||
| Impact Pacific | |||
| Planned sequence | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| T+2:28 MECO | |||
| T+2:39 Stage 1 sep | |||
| T+2:43 St 2 burn, | |||
| T+2:48 At 100 km | |||
| T+3:13 Fairing sep | |||
| T+9:37 SECO | |||
| T+9:47 Trailblazer sep | |||
| T+13:57 PRESat sep | |||
| T+18:07 NanoSail-D sep | |||
No comments:
Post a Comment