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15Zh58A
MITT solid rocket engine. Topol'-M first stage.

AKA: Topol'-M-1. Status: Active. Thrust: 980.00 kN (220,310 lbf). Gross mass: 26,000 kg (57,000 lb). Unfuelled mass: 3,000 kg (6,600 lb). Burn time: 60 s. Height: 8.50 m (27.80 ft). Diameter: 1.80 m (5.90 ft).

Subtopics

RD RT-21 (1) MITT solid rocket engine. Temp-2S first stage.

MIHT-1 MIHT solid rocket engine. Start-1. In production. Used in Start-1. Estimated values. First flight 1993. Solid propellant rocket stage. All estimated. Start first stage.

People: Nadiradze. Country: Russia. Launch Vehicles: Topol'-M, Bulava. Propellants: Solid. Stages: 15Zh58A.

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