15D13
11D513A
Credit - © Dietrich Haeseler
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 and Further Reading
  • Yeteyev, Ivan, Operezhaya vremya, Ocherki, Moscow, 1999.. Collection of articles involving the life and works of Chief Designer Chelomei and the Khrunichev factory.
 
 
 
 
 
 
 
 
 
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