Isayev Nitric acid/Amine rocket engine. 167 kN. SAM-missiles 217M and 218. Out of Production. Designation unknown.
Application: SAM-missiles 217M and 218.
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.
Status: Out of Production.
More... - Chronology...
Unfuelled mass: 122 kg (268 lb).
Height: 1.02 m (3.33 ft).
Diameter: 0.62 m (2.05 ft).
Thrust: 167.00 kN (37,543 lbf).
First Launch: 1950s late.
Associated Launch Vehicles
217 Russian surface-to-air missile. The 217 was a version of the V-300 with a variable thrust engine. Entered production. More...
Associated Manufacturers and Agencies
Nitric acid/Amine Drawing on the German World War II Wasserfall rocket, nitric acid (HNO3) became the early storable oxidiser of choice for missiles and upper stages of the 1950's. To overcome various problems with its use, it was necessary to combine the nitric acid with N2O4 and passivation compounds. These formulae were considered extremely secret at the time. By the late 1950's it was apparent that N2O4 by itself was a better oxidiser. Therefore nitric acid was almost entirely replaced by pure N2O4 in storable liquid fuel rocket engines developed after 1960. Early storable rocket systems sought to improve ignition characteristics and perforamance by eliminating the kerosene portion of the fuel. An amine is an organic compound produced when one or more hydrogen atoms of ammonia is replaced with organic groups. Mixed amine fuels were first developed by the Germans in World War II. TONKA-250, developed for the Wasserfall rocket, was used by the Russians after the war in various engines under the specification TG-02. More...
Russian Arms Catalogue, Vol 5 and 6, Military Parade, Moscow via Dietrich Haeseler.
Siddiqi, Asif A, Soviet Space Web Page, 1999 via Dietrich Haeseler. Web Address when accessed: here.
Home - Browse - Contact
© / Conditions for Use