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15D23P
Part of 15D23
TsKB-7 solid rocket engine. RT-2P Stage 1. Out of Production. Three gimbaled nozzles for steering. Ammonium perchlorate/ammonium butyl propellant. Chamber pressure 56 kgf/cm2.

Status: Out of Production. Date: 1968-1972. Number: 4 . Thrust: 980.00 kN (220,310 lbf). Gross mass: 34,550 kg (76,160 lb). Unfuelled mass: 3,750 kg (8,260 lb). Burn time: 75 s. Height: 9.20 m (30.10 ft). Diameter: 1.84 m (6.03 ft).

Country: Russia. Launch Vehicles: RT-2P, RT-2M. Propellants: Solid. Stages: 15D23P. Agency: Arsenal, TsKB-7.
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