UA-156 Designer: United Technologies. Gross Mass: 544,311 kg (1,200,000 lb). Empty Mass: 37,195 kg (82,000 lb). Propellants: Solid. Thrust(vac): 8,924.300 kN (2,006,262 lbf). Thrust(sl): 8,076.000 kN (1,815,557 lbf). Isp: 263 sec. Isp (sea level): 238 sec. Burn time: 157 sec. Diameter: 3.96 m (12.99 ft). Length: 34.00 m (111.00 ft). Chambers: 1. Country: USA. Status: Study 1968. UA-156 used on Rocket Stages Used on stage: UA 156 inch. on launch vehicle: Saturn V-25(S)B. Used on stage: UA 156 inch. on launch vehicle: Saturn V-25(S)U. Used on stage: UA 156 inch 4 Segment. on launch vehicle: Saturn INT-27.                   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 - 2007 except where otherwise noted.

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