RetroSearch Browse

Home - News ( United States | United Kingdom | Italy | Germany ) - Football scores

Showing content from http://www.astronautix.com/c/../s/../r/../r/rd-0242.html below:

RD-0242

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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-0242 RD-0242 Credit: KBKhA Kosberg N2O4/UDMH rocket engine. sea-based missile booster stage developed 1977-83 (Burlak). First concept planned N2O4/kerosene as propellant, but changed to N2O4/UDMH. Single ignition, 297 development tests. 50 engines for sale. Status: Developed 1977-83. Date: 1977-83. Thrust: 123.60 kN (27,786 lbf). Unfuelled mass: 120 kg (260 lb). Specific impulse: 303 s. Burn time: 60 s. Height: 0.88 m (2.89 ft). Diameter: 0.27 m (0.89 ft). Max. duration 420 s. Engine: 120 kg (260 lb). Chamber Pressure: 196.20 bar. Thrust to Weight Ratio: 105.03. Subtopics RD-0242-HC Kosberg LOx/Kerosene rocket engine. Developed 1998-. Proposed variant of RD-0242 engine using LOX-kerosene instead of N2O4/UDMH as propellants. RD-0242M Kosberg N2O4/MMH rocket engine. Design concept 1998-. Proposed variant of RD-0242 engine for upper stages using MMH in place of UDMH. Reusable for 6 ignitions total. Throttling to 80%. RD-0242M1 Kosberg N2O4/MMH rocket engine. Design concept 1998-. Proposed variant of RD-0242 engine for upper stages using MMH in place of UDMH (adaptation to western market). Reusable for 6 ignitions total. Throttling to 80%. Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Kosberg bureau. Bibliography: 312, 342, 95. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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 © 1997-2019 Mark Wade - Contact © / Conditions for Use

RetroSearch is an open source project built by @garambo | Open a GitHub Issue

Search and Browse the WWW like it's 1997 | Search results from DuckDuckGo

HTML: 3.2 | Encoding: UTF-8 | Version: 0.7.4