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S5.1


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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 S5.1 Isayev Nitric acid/Amine rocket engine. SAM-missiles 217M and 218. Out of Production. Designation unknown.

Status: Out of Production. First Launch: 1950s late. Thrust: 167.00 kN (37,543 lbf). Unfuelled mass: 122 kg (268 lb). Height: 1.02 m (3.33 ft). Diameter: 0.62 m (2.05 ft).

Throttled thrust(vac): 49.000 kN (11,015 lbf). Engine: 122 kg (268 lb). Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 139.34.

Family: Storable liquid. Country: Russia. Launch Vehicles: 217 missile. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 342, 344. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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