
Trailblazer [SpaceDev]
The Trailblazer spacecraft used a satellite bus originally developed under a Missile Defense Agency contract. Trailblazer demonstrated a flexible, modular commercial bus design using off the shelf components.
Trailblazer was one of the three candidate payloads for the quick reaction "Jumpstart" launch in 2008 on a Falcon-1 launch vehicle. Trailbazer was selected only a few weeks before launch.
The satellite failed to reach orbit due to a launch vehicle first stage malfunction.
| Nation: | USA |
|---|---|
| Type / Application: | Technology |
| Operator: | |
| Contractors: | SpaceDev |
| Equipment: | |
| Configuration: | MMB-100 Bus |
| Propulsion: | None |
| Power: | |
| Lifetime: | |
| Mass: | 83.5 kg |
| Orbit: |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| Trailblazer | 03.08.2008 | Om | F | Falcon-1 | with PreSat, Nanosail D, Celestis 07 |