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/../s/saturnint-21.html below:

Saturn INT-21


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 Saturn INT-21 Part of Saturn V

Saturn V Skylab
Credit: NASA
American orbital launch vehicle. Saturn variant consisting of S-IC first stage and S-II second stage. This essentially flew once to launch Skylab in 1972, although the IU was located atop the Skylab space station (converted S-IVB stage) rather than atop the S-II as in the INT-21 design.

Status: Study 1967. Payload: 115,900 kg (255,500 lb). Thrust: 33,737.90 kN (7,584,582 lbf). Gross mass: 2,916,080 kg (6,428,850 lb). Height: 80.00 m (262.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

Liftoff Mass - kg S-IC - No. F-1 Motors S-II - No. J-2 Motors Payload - kg - 4.68 G limit 2,209,000 4 3 76,000 2,209,000 4 4 84,000 2,209,000 4 5 89,000 2,762,000 5 3 101,000 2,762,000 5 4 112,000 2,762,000 5 5 116,000

LEO Payload: 115,900 kg (255,500 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 681.500 million.

Stage Data - Saturn INT-21

Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1. Spacecraft: Space Station 1970. Stages: Saturn IC, Saturn II. Photo Gallery S-1C details
Credit: © Mark Wade Saturn II stage
Credit: © Mark Wade 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