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/rombuscore.html below:

Rombus core


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 Rombus core Part of Rombus LOx/LH2 propellant rocket stage. 36 x plug-nozzle engines (20 atm chamber pressure, 7:1 mixture ratio).

AKA: Rombus. Status: Study 1964. Thrust: 101,900.00 kN (22,908,000 lbf). Gross mass: 5,102,041 kg (11,248,075 lb). Unfuelled mass: 306,175 kg (675,000 lb). Specific impulse: 455 s. Specific impulse sea level: 359 s. Burn time: 215 s. Height: 28.96 m (95.01 ft). Diameter: 16.00 m (52.00 ft). Span: 24.39 m (80.01 ft).

Cost $ : 50.000 million.

Country: USA. Engines: Plug-Nozzle Rombus. Launch Vehicles: Rombus. Propellants: Lox/LH2. 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