Start-1
Start familyMoscow Institute of Thermal TechnologyRetired
Start-1 is a Russian satellite launch vehicle based on the RT-2PM Topol, a Soviet intercontinental ballistic missile developed by Moscow Institute of Thermal Technology.
Specifications
- Thrust
- 887 kN
- Height
- 22.7 m
- Diameter
- 1.61 m
- Launch mass
- 47 t
- Stages
- 4
- Launch cost
- $9M
- LEO capacity
- 632 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
5flightswith a definitive outcome
100%success rate5 of 5
0failuresincluding partial failures
5success streakcurrent
First flight March 25, 1993 · latest April 25, 2006
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Start-1 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1993 | 1 | 0 | 1 |
| 1994 | 0 | 0 | 0 |
| 1995 | 0 | 0 | 0 |
| 1996 | 0 | 0 | 0 |
| 1997 | 1 | 0 | 1 |
| 1998 | 0 | 0 | 0 |
| 1999 | 0 | 0 | 0 |
| 2000 | 1 | 0 | 1 |
| 2001 | 1 | 0 | 1 |
| 2002 | 0 | 0 | 0 |
| 2003 | 0 | 0 | 0 |
| 2004 | 0 | 0 | 0 |
| 2005 | 0 | 0 | 0 |
| 2006 | 1 | 0 | 1 |