A RetroSearch Logo

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

Search Query:

Showing content from http://www.astronautix.com/c/../s/../r/../r/r-36-1.html below:

R-36-1


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 R-36-1 N2O4/UDMH propellant rocket stage. Verniers 4 x RD-68M, 285 kN, maximum 42 degree gimbal angle.

AKA: R-36--1. Status: Retired 1975. Thrust: 2,651.70 kN (596,126 lbf). Gross mass: 122,300 kg (269,600 lb). Unfuelled mass: 6,400 kg (14,100 lb). Specific impulse: 301 s. Specific impulse sea level: 269 s. Burn time: 120 s. Height: 18.90 m (62.00 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 6.000 million.

Subtopics R-36-0-1 N2O4/UDMH propellant rocket stage. . R-36M-1 N2O4/UDMH rocket stage. 4522.00 kN (1,016,586 lbf) thrust. Mass 210,000 kg (462,971 lb). Tsyklon 2-1 N2O4/UDMH propellant rocket stage. SL-11; 11K68;R-36M. Tsyklon 3-1 N2O4/UDMH propellant rocket stage. SL-14;11K69. Country: Ukraine. Engines: RD-251. Launch Vehicles: R-36 8K67, Tsiklon, Tsiklon-2A, R-36 8K67M, R-36 8K67P, R-36 8K67MA, R-36 8K67PM. Propellants: N2O4/UDMH. 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