RDMT-0.8
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Engine: 0.10 kg (0.22 lb). Thrust to Weight Ratio: .81.
Related
- Family
- Cold Gas
- Country
- Russia
- Propellants
- Nitrogen+Helium
- Agency
- NII Mash
- Bibliography
- 336