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RD R-29 (1)


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RD R-29 (1) Part of RD-0243 Makeyev N2O4/UDMH rocket engine.

Thrust: 682.00 kN (153,319 lbf). Burn time: 74 s.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Vysota-1. Agency: Makeyev bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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