Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

---

Soyuz M-1

---

Status: Development ended 2000. Thrust: 872.00 kN (196,033 lbf). Gross mass: 100,500 kg (221,500 lb). Unfuelled mass: 6,000 kg (13,200 lb). Specific impulse: 336 s. Specific impulse sea level: 298 s. Burn time: 310 s. Height: 28.00 m (91.00 ft). Diameter: 2.95 m (9.67 ft). Span: 2.95 m (9.67 ft).