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11D513A
Credit - © Dietrich Haeseler
Engine Model: 15D13. Designer: Klimov. Propellants: N2O4/UDMH. Thrust(vac): 131.400 kN (29,540 lbf). Chambers: 1. Country: USSR. Status: Study 1968.

Main engine for midcourse Block 1V ascent/trans-earth injection stage of LK-700 manned spacecraft. See also 11D423.

Bibliography:

  • Yeteyev, Ivan, Operezhaya vremya, Ocherki, Moscow, 1999..
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