“Saturn IB-D”的意思、由来-开放百科全书

词条

Saturn IB-D

释义

References

{{Infobox rocket
|name = Saturn IB-D
|function = Unmanned LEO and Lunar launch vehicle
|manufacturer = Von Braun
|country-origin = United States
|height = 51.00 m
|alt-height = 167.00 ft
|diameter = 6.61 m
|alt-diameter = 21.68 ft
|mass = 1,511,980 kg
|alt-mass = 3,333,340 lb
|stages = 3
|LEO-payload =33,000 kg
|alt-LEO =72,000 lb
|status = Concept/study
|sites = N/A
|launches = N/A
|stage1name = 4x Titan UA1205
|stage1engines = United Technologies UA1205 solid motor
|stage1thrust = 5,849.411 kN
|alt-stage1thrust = 1,315,000 lb_f
|stage1time = 115 seconds
|stage1fuel = Solid
|stage2name = S-1B
|stage2engines = 8 Rocketdyne H-1
|stage2thrust = 8,241.763 kN
|alt-stage2thrust = 1,852,822 lb_f
|stage2time = 155 seconds
|stage2fuel = RP-1/LOX
|stage3name = S-IVB
|stage3engines = 1 Rocketdyne J-2
|stage3thrust = 1,031.600 kN
|alt-stage3thrust = 231,913 lb_f
|stage3time = 475 seconds
|stage3fuel = LH2/LOX
}}

Studied by Douglas Aircraft Company in 1965, this rocket consisted of a whole Saturn IB with 4 strap-on SRBs that have flown on the Titan 3E interplanetary missile carriers. All components of the vehicle have flown, but not together for this concept.

References

Lowther, Scott, Saturn: Development, Details, Derivatives and Descendants, Work in progress. Available chapters may be ordered directly from Scott Lowther at web site indicated. Accessed at: https://web.archive.org/web/20070521083808/http://www.webcreations.com/ptm.

1 : Saturn (rocket family)

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