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)