A RetroSearch Logo

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

Search Query:

Showing content from http://www.astronautix.com/c/../s/../s/../l/../r/rd-0109.html below:

RD-0109


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-0109 Part of S1
RD-0109
Credit: KBKhA Kosberg LOx/Kerosene rocket engine. 8A92 Vostok stage 3, 8K72K stage 3 (block E-Vostok). Out of production. Developed in 15 months. First flight 1960.

AKA: 8D719;RD-448;RD-448, RO-7;RO-7. Status: Out of production. Date: 1959-60. Number: 154 . Thrust: 54.52 kN (12,257 lbf). Unfuelled mass: 121 kg (266 lb). Specific impulse: 324 s. Burn time: 430 s. Height: 1.58 m (5.18 ft). Diameter: 0.76 m (2.49 ft).

Engine: 121 kg (266 lb). Chamber Pressure: 50.00 bar. Area Ratio: 79.4. Propellant Formulation: Lox/RG-1. Thrust to Weight Ratio: 45.95.

Country: Russia. Launch Vehicles: Vostok 8K72K, Vostok 8A92, Vostok 8A92M. Propellants: Lox/Kerosene. Stages: Vostok 8K72K-2, Vostok 8A92-2, Vostok 8A92M-2. Agency: Kosberg bureau. Bibliography: 307, 320, 95, 7466. 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