OTRAG (rocket)
| Function | Launch vehicle |
|---|---|
| Manufacturer | OTRAG |
| Country of origin | Germany |
| Launch history | |
| Status | Retired |
| Launch sites | Shaba North, Congo Sabha, Libya Esrange, Sweden |
| Total launches | 18 |
| First flight | 18 May 1977 |
| Last flight | 19 September 1983 |
| Common Rocket Propulsion Unit | |
| Height | 16 m (52 ft) |
| Diameter | 0.27 m (11 in) |
| Empty mass | 150 kg (330 lb) |
| Gross mass | 1,500 kg (3,300 lb) |
| Powered by | 1 × OTRAG |
| Maximum thrust | 26.960 kN (6,061 lbf) |
| Specific impulse | 297 s (2.91 km/s) |
| Burn time | 140 seconds |
| Propellant | N2O4 |
The OTRAG rocket was a modular satellite-delivery rocket developed by the OTRAG company in the 1970s and 80s. The OTRAG rocket was to become a rocket built up from several mass-produced units, intended to carry satellites with a weight of 1-10 tons or more into orbit. Mass production meant that the vehicle was projected to have been 10x cheaper than conventional vehicles of similar capability.