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/ssmestudy.html below:

SSME Study


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 SSME Study Part of SSME Notional LOx/LH2 rocket engine. Study 1967.

Status: Study 1967. Thrust: 1,535.20 kN (345,127 lbf). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 379 s.

Thrust (sl): 1,200.700 kN (269,928 lbf). Thrust (sl): 122,443 kgf.

Country: USA. Launch Vehicles: S series sounding rockets, Spacemaster, Shuttle FR-3, Shuttle LS A, Shuttle NAR A, Shuttle MDC, Shuttle HCR, Shuttle LCR, Shuttle DC-3, Shuttle R134C, Shuttle LS200, Shuttle H33. Propellants: Lox/LH2. Stages: Spacemaster-1, Spacemaster-2, Shuttle FR-3-1, Shuttle FR-3-2, Shuttle HCR-1, Shuttle HCR-2, Shuttle LCR-1, Shuttle LCR-2, Shuttle LS A-1, Shuttle LS A-2, Shuttle MDC-A-1, Shuttle MDC-A-2, Shuttle NAR A-1, Shuttle NAR A-2, Shuttle DC-3-1, Shuttle DC-3-2, Shuttle R134C-1, Shuttle R134C-2, Shuttle R134G-1, Shuttle R134G-2, Shuttle H33-1, Shuttle H33-2, Shuttle LS200-1. 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