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/saturna-2.html below:

Saturn A-2


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 A-2 Part of Saturn I
Saturn A-2
Credit: © Mark Wade
American orbital launch vehicle. More powerful version of Saturn I with low energy second stage consisting of cluster of four IRBM motors and tankage, Centaur third stage. Masses, payload estimated.

Status: Study 1959. Payload: 10,000 kg (22,000 lb). Thrust: 7,295.10 kN (1,640,004 lbf). Gross mass: 702,960 kg (1,549,760 lb). Height: 62.00 m (203.00 ft). Diameter: 6.52 m (21.39 ft). Apogee: 185 km (114 mi).

LEO Payload: 10,000 kg (22,000 lb) to a 185 km orbit at 38.00 degrees. Payload: 2,000 kg (4,400 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 63.800 million.

Stage Data - Saturn A-2

Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: S-3, H-1b, RL-10A-1. Stages: Jupiter Cluster, Centaur C, Saturn IB stage. Photo Gallery Saturn A-1 to C-5
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