Saturn INT-21

The Saturn INT-21 was an American orbital launch vehicle of the 1970s. It was derived from the Saturn V rocket used for the Apollo program, and is casually referred to as a "modified Saturn V." It was only launched once, from Kennedy Space Center at Cape Canaveral, carrying the Skylab space station into orbit, at 17:30 GMT, on May 14, 1973. It was intended to be used for other flights in the Apollo Applications Program, and would have also been u... more

Rocket

Country Of Origin:

Maiden Flight:

  • May 14, 1973

Last Flight:

  • May 14, 1973

Height:

  • 80 m (260 ft )

Diameter:

  • 10 m (33 ft )

Mass:

  • 2,916,000 kg (6428680 lb )

Number Of Stages:

  • 2

Status:

Stages:

Stage Number Engine Thrust (newtons) Burn Time (seconds) Fuels
  • 2
  • 5,000,000 N (36165070 pdl )
  • 6 min
  • 1
  • 34,020,000 N (246067130 pdl )
  • 2 min 30 s
View entire collection »
top ↑

These people have edited this topic:

Edit this topic
Edit and Show details

Add or delete facts, download data in JSON or RDF formats, and explore topic metadata.

Freebase Logo
What is Freebase?

Freebase is a huge collection of facts, built by people like you. Freebase connects facts in ways other sites can't, giving you new ways to explore millions of subjects.
You can help improve it!

Freebase Attribution

Freebase data is free for use under the CC-BY license.

The original description for Saturn INT-21 was automatically generated from Wikipedia.org licensed under the GNU Free Documentation License.
[1]
Learn more about Freebase licensing and attribution