Encyclopedia Astronautica
Start-1


Solid propellant rocket stage. Loaded/empty mass 26,000/3,000 kg. Thrust 980.00 kN. Vacuum specific impulse 263 seconds. All estimated

Cost $ : 4.000 million.

Status: Active.
Gross mass: 26,000 kg (57,000 lb).
Unfuelled mass: 3,000 kg (6,600 lb).
Height: 8.50 m (27.80 ft).
Diameter: 1.61 m (5.28 ft).
Span: 1.61 m (5.28 ft).
Thrust: 980.00 kN (220,310 lbf).
Specific impulse: 263 s.
Specific impulse sea level: 238 s.
Burn time: 60 s.
Number: 58 .

More... - Chronology...


Associated Countries
Associated Engines
  • MIHT-1 MIHT solid rocket engine. 980.6 kN. Start-1. In production. Used in Start-1. Estimated values. Isp=263s. First flight 1993. More...

Associated Launch Vehicles
  • Topol Russian containerised all-solid propellant intercontinental ballistic missile designed for launch from mobile and silo launchers. Replaced UR-100/UR-100NU in silos. More...
  • Start-1 Russian orbital launch vehicle. Launch vehicle based on decommissioned ICBM's. Launched from mobile transporter. Liftoff mass 47 tonnes. More...
  • Start Russian orbital launch vehicle. Launch vehicle based on decommissioned SS-25 ICBM's (differs from ICBM/basic Start-1 in having second stage used twice, in tandem, for increased payload). Launched from mobile transporter. Liftoff mass 60 tonnes. More...

Associated Propellants
  • Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

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