The RD-861 is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a main combustion...

experience had been mostly on hypergolic propellants engines, like the RD-855 or RD-861, they were considered too toxic for modern ecological standards. While...

the RD-120 nozzle can pass through. Whilst Yuzhnoye's propulsion experience had been mostly on hypergolic propellants engines, like RD-855 or RD-861, they...

July 27, 2019. "RD-107A and RD-108A". NPO Energomash. Retrieved June 30, 2015. "RD-171M". NPO Energomash. Retrieved June 30, 2015. "RD-180". NPO Energomash...

1 RD-252 Maximum thrust 940 kN (210,000 lbf) Specific impulse 317 sec Burn time 160 seconds Propellant N2O4 / UDMH Third stage Powered by 1 RD-861 Maximum...

160 seconds Propellant N2O4 / UDMH Third stage – 11S693 Powered by 1 RD-861 Maximum thrust 78.7 kN (17,700 lbf) Specific impulse 317 sec Burn time 125...

Show map of the United States Location ME 161 S side, .1 mi. E of private rd. 861, St. John, Maine Coordinates 47°12′31″N 68°48′19″W / 47.20861°N 68.80528°W...

updated its study plan in accordance with the Bologna Process (RD 1393/2007 (modificado por RD 861/2010) for both undergraduate and postgraduate studies. Degree...

Molecular Cell. 2 (6): 851–861. doi:10.1016/S1097-2765(00)80299-3. PMID 9885572. Zhang Y, Yinghua L (2010). "The Expanding Mi-2/NuRD Complexes: A Schematic...

Evidence from the EIB Investment Survey. European Investment Bank. ISBN 978-92-861-5233-7. "Press corner". European Commission – European Commission. Retrieved...