| Apollo LES |
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Model: Apollo LES-1. Gross Mass: 2,500 kg (5,500 lb). Thrust (vac): 690.000 kN (155,110 lbf). Burn time: 3.00 sec. Propellants: Solid. Diameter: 0.66 m (2.16 ft). Length: 10.20 m (33.40 ft). Country: USA. No Engines: 1. Motor: LPC A-1. Status: Retired 1965. Used as: Apollo LES. Other designations: LES.
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