Energia M - Energia M in static test building Credit: © Mark Wade. 21,058 bytes. 299 x 447 pixels.

Launch vehicle using surplus Energia components to put medium size payloads in orbit. Abandoned (no customers, boosters built in Ukraine).

LEO Payload: 34,000 kg. to: 200 km Orbit. Liftoff Thrust: 1,633,160 kgf. Total Mass: 1,022,800 kg. Core Diameter: 7.7 m. Total Length: 24.0 m. Flyaway Unit Cost $: 80.00 million. in 1985 unit dollars.

• Stage Number: 0. 2 x Energia Strapon Gross Mass: 355,000 kg. Empty Mass: 35,000 kg. Thrust (vac): 806,200 kgf. Isp: 337 sec. Burn time: 145 sec. Isp(sl): 309 sec. Diameter: 3.9 m. Span: 4.2 m. Length: 37.7 m. Propellants: Lox/Kerosene No Engines: 1. RD-170

• Stage Number: 1. 1 x Energia M Gross Mass: 272,000 kg. Empty Mass: 28,000 kg. Thrust (vac): 200,000 kgf. Isp: 455 sec. Burn time: 550 sec. Isp(sl): 352 sec. Diameter: 7.7 m. Span: 7.7 m. Length: 20.0 m. Propellants: Lox/LH2 No Engines: 1. RD-0120M

• 42 - Isakowitz, Steven J,, International Reference to Space Launch Systems Second Edition, AIAA, Washington DC, 1991.
• 89 - Semenov, Yu. P., S P Korolev Space Corporation Energia, RKK Energia, 1994.

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Energia M Credit: © Mark Wade. 2,958 bytes. 93 x 309 pixels.

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Energia M on Pad Credit: RKK Energia. 27,285 bytes. 308 x 240 pixels.

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Energia M Rollout Credit: RKK Energia. 21,149 bytes. 307 x 237 pixels.

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