HVAR

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Engine Model: HVAR. Designer: CIT. Gross Mass: 40 kg (88 lb). Empty Mass: 17 kg (37 lb). Propellants: Solid. Thrust(vac): 25.000 kN (5,620 lbf). Burn time: 0.90 sec. Diameter: 0.13 m (0.42 ft). Length: 1.70 m (5.50 ft). Country: USA. HVAR used on Rocket Stages Used on stage: HVAR. on launch vehicle: Deacon. Used on stage: HVAR. on launch vehicle: HVAR. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.