HeadlessSeeker
GA Member
- Jul 1, 2018
- 2,823
| TYPE | Research & Development |
| COUNTRY | Russia |
| PROJECT | Start-1 |
| PROJECT COST | 1,000,000,000.00 |
| COMPLETION DATE | 02/07/2020 |
| PROJECT INFORMATION | https://en.wikipedia.org/wiki/Start-1 http://www.astronautix.com/s/start-1.html Function Small orbital launch vehicle Manufacturer Moscow Institute of Thermal Technology Country of origin Russia Size Height 22.7 m (74 ft) Diameter 1.8 m (5.9 ft) Mass 47,200 kg (104,100 lb) Stages 4 Capacity Payload to LEO 550 kg (1,393 lb) Payload to SSO 167 kg (368 lb) First stage - Start-1 Engines 1 MIHT-1 Thrust 980 kN (220,310 lbf) Specific impulse 263 s Burn time 60 s Propellant Solid Second stage Start-2 Engines 1 MIHT-2 Thrust 490 kN (110,150 lbf) Specific impulse 280 s Burn time 64 s Propellant Solid Third stage - Start-3 Engines 1 MIHT-3 Thrust 245 kN (55,078 lbf) Specific impulse 280 s Burn time 56 s Propellant Solid Fourth stage - Start-4 Engines 1 MIHT-4 Thrust 9.8 kN (2,203 lbf) Specific impulse 295 s Burn time 207 s Propellant Solid “Start-1.” Wikipedia, Wikimedia Foundation, 6 May 2020, en.wikipedia.org/wiki/Start-1. |
| PRIVATE / ENCRYPTED | No |
