Phobos EAV
General Specifications | |
Diameter | 4 inches (104mm) |
Length | 13 feet (3.96m) |
Recovery | Parachute at apogee (booster) Parachute at apogee (upper section) Parachute at 1000 feet (upper section) |
Fin Geometry | |
Nosecone | Conical |
Motor | |
Motor Type | Kosdon O-10,000 |
Total Impulse | 22,000 Newton seconds |
Nozzle | Pyrolytic Graphite |
Burn Time | 2.4 seconds |
Avionics & Payloads | |
Avionics (Upper Stage) | |
Avionics (Booster) |
Thrust Curve from the Kosdon O-10,000 Solid Rocket Motor used for the Phobos EAV Flight.
(Note: the data is taken directly from the R-DAS Flight Computer data carried onboard the Phobos EAV rocket - sampled at 200 Hz)