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/saturnivbs-ib.html below:

Saturn IVB (S-IB)


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 IVB (S-IB) Part of Saturn IV LOx/LH2 propellant rocket stage. Saturn IB version of S-IVB stage. Due to lower payload, 300 kg saving in structure compared to Saturn V version. Due to deletion of restart requirement, 700 kg saving in propulsion system (primarily reduction in helium for restart).

Status: Study 1967. Thrust: 1,031.60 kN (231,913 lbf). Gross mass: 118,800 kg (261,900 lb). Unfuelled mass: 12,900 kg (28,400 lb). Specific impulse: 421 s. Specific impulse sea level: 200 s. Burn time: 475 s. Height: 17.80 m (58.30 ft). Diameter: 6.61 m (21.68 ft). Span: 6.61 m (21.68 ft).

Country: USA. Engines: J-2. Launch Vehicles: Saturn IB, Saturn INT-05, Saturn INT-27, Saturn INT-05A, Saturn IB-C, Saturn IB-CE, Saturn IB-D, Uprated Saturn I, Saturn INT-11, Saturn INT-12, Saturn INT-13, Saturn INT-14, Saturn INT-15, Saturn INT-16, Saturn INT-17, Saturn INT-18, Saturn INT-19, Saturn V, Saturn LCB-Alumizine-140, Saturn LCB-Alumizine-250, Saturn LCB-Storable-140, Saturn LCB-Storable-250, Saturn LCB-Lox/RP-1, Saturn S-IC-TLB, Saturn LCB-SR. 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