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- Saturn_II diameter "10.0584".
- Saturn_II height "50901.6".
- Saturn_II mass "328406.4".
- Saturn_II lowerEarthOrbitPayload "21319.2".
- Saturn_II mass "328406.4".
- Saturn_II abstract "The Saturn II was a series of proposed American Expendable launch vehicles, proposed by North American Aviation in 1966, derived from the Saturn V rocket that was used for the Apollo lunar program.There was a large payload gap between the Saturn IB's 19,000 kg low-earth orbit capacity and the two-stage Saturn V's 100,000 kg capability. In the mid-1960s NASA's Marshall Space Flight Center (MSFC) initiated several studies to extend the capabilities of the Saturn family. The studies examined a number of Modified Launch Vehicle (MLV) configurations based on the Saturn IB and Saturn V launch vehicles as well as Intermediate Payload (INT) launch vehicles based on modified Saturn stages (MS-IB, MS-IC, MS-II, and MS-IVB). Martin Marietta (builder of Atlas, Titan vehicles), Boeing (builder of S-1B and S-1C first stages) and North American (builder of the S-II second stage) were three of the companies that provided responses.North American considered the best way to fill the gap was to use the Saturn V's second stage, the S-II, as the first stage of an intermediate launch vehicle.The basic concept of the Saturn II was to save money by ceasing production of the Saturn IB rocket, and replacing it with launch vehicles built entirely with current Saturn V components. This would allow closing down production lines for the S-IB first stage, and would allow for more efficient integration of rocket systems.It would have replaced the Saturn IB, which had a maximum payload capability of 46,000 pounds (21,000 kg), for launching spacecraft into low Earth orbit.".
- Saturn_II countryOrigin United_States.
- Saturn_II diameter "10.0584".
- Saturn_II height "50.9016".
- Saturn_II launchSite Kennedy_Space_Center.
- Saturn_II launchSite Kennedy_Space_Center_Launch_Complex_39.
- Saturn_II lowerEarthOrbitPayload "2.13192E7".
- Saturn_II manufacturer Douglas_Aircraft_Company.
- Saturn_II manufacturer North_American_Aviation.
- Saturn_II mass "3.284064E8".
- Saturn_II rocketFunction Launch_vehicle.
- Saturn_II rocketStages "2".
- Saturn_II status "1967 Study".
- Saturn_II status "Cancelled".
- Saturn_II thumbnail Saturn_II.svg?width=300.
- Saturn_II totalLaunches "0".
- Saturn_II wikiPageExternalLink satvint.pdf.
- Saturn_II wikiPageExternalLink saturnii.htm.
- Saturn_II wikiPageID "6597242".
- Saturn_II wikiPageRevisionID "588315603".
- Saturn_II caption "Saturn II proposals: Left to right, INT-17, 18 and 19.".
- Saturn_II countryOrigin United_States.
- Saturn_II function "Orbital launch vehicle".
- Saturn_II hasPhotoCollection Saturn_II.
- Saturn_II launches "0".
- Saturn_II manufacturer North_American_Aviation.
- Saturn_II manufacturer "Douglas".
- Saturn_II name "Saturn II".
- Saturn_II sites Kennedy_Space_Center.
- Saturn_II sites Kennedy_Space_Center_Launch_Complex_39.
- Saturn_II stage1engines "5".
- Saturn_II stage1fuel Liquid_hydrogen.
- Saturn_II stage1fuel Liquid_oxygen.
- Saturn_II stage1name S-II.
- Saturn_II stage1time "360.0".
- Saturn_II stage2engines "1".
- Saturn_II stage2fuel Liquid_hydrogen.
- Saturn_II stage2fuel Liquid_oxygen.
- Saturn_II stage2name S-IVB.
- Saturn_II stage2time "400.0".
- Saturn_II stages "2".
- Saturn_II status "1967".
- Saturn_II status "Cancelled".
- Saturn_II subject Category:Saturn_(rocket_family).
- Saturn_II type Artifact100021939.
- Saturn_II type Conveyance103100490.
- Saturn_II type Instrumentality103575240.
- Saturn_II type Object100002684.
- Saturn_II type PhysicalEntity100001930.
- Saturn_II type Rocket104099429.
- Saturn_II type Vehicle104524313.
- Saturn_II type Whole100003553.
- Saturn_II type MeanOfTransportation.
- Saturn_II type Rocket.
- Saturn_II type RocketEngine.
- Saturn_II type DesignedArtifact.
- Saturn_II comment "The Saturn II was a series of proposed American Expendable launch vehicles, proposed by North American Aviation in 1966, derived from the Saturn V rocket that was used for the Apollo lunar program.There was a large payload gap between the Saturn IB's 19,000 kg low-earth orbit capacity and the two-stage Saturn V's 100,000 kg capability. In the mid-1960s NASA's Marshall Space Flight Center (MSFC) initiated several studies to extend the capabilities of the Saturn family.".
- Saturn_II label "Saturn II".
- Saturn_II sameAs m.0gd4gt.
- Saturn_II sameAs Q7426795.
- Saturn_II sameAs Q7426795.
- Saturn_II sameAs Saturn_II.
- Saturn_II wasDerivedFrom Saturn_II?oldid=588315603.
- Saturn_II depiction Saturn_II.svg.
- Saturn_II isPrimaryTopicOf Saturn_II.
- Saturn_II name "Saturn II".
