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- Saturn_C-3 diameter "8.128".
- Saturn_C-3 height "81991.2".
- Saturn_C-3 mass "464336.712".
- Saturn_C-3 mass "464336.712".
- Saturn_C-3 abstract "The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kg (100,000 lb) to low Earth orbit and send 18,000 kg (39,000 lb) to the Moon via Trans-Lunar Injection.President Kennedy's proposal on May 25, 1961 of an explicit manned lunar landing goal spurred NASA to concretize its launch vehicle requirements for a lunar landing. A week earlier, William Fleming (Office of Space Flight Programs, NASA Headquarters) chaired an ad hoc committee to conduct a six-weeks study of the requirements for a lunar landing. Judging the direct ascent approach to be the most feasible, they concentrated their attention accordingly, and proposed circumlunar flights in late 1965 using the Saturn C-3 launch vehicle.In early June 1961, Bruce Lundin, deputy director of the Lewis Research Center, led a week-long study of six different rendezvous possibilities. The alternatives included earth-orbital rendezvous, lunar-orbital rendezvous, earth and lunar rendezvous, and rendezvous on the lunar surface, employing Saturn C-1s, C-3s, and Nova designs. Lundin's committee concluded that rendezvous enjoyed distinct advantages over direct ascent and recommended an earth-orbital rendezvous using two or three Saturn C-3s.NASA announced on September 7, 1961 that the government-owned Michoud Ordnance Plant near New Orleans, LA, would be the site for fabrication and assembly of the Saturn C-3 first stage as well as larger vehicles in the Saturn program. Finalists were two government-owned plants in St. Louis and New Orleans. The height of the factory roof at Michoud meant that an 8 x F-1 engined launch vehicle (Nova class, Saturn C-8) could not be built; 4 or 5 engines would have to be the maximum.This decision ended consideration of a Nova class launch vehicle for Direct Ascent to the Moon or as heavy-lift companion with the Saturn C-3 for Earth Orbit Rendezvous.".
- Saturn_C-3 comparable Delta_IV_Heavy.
- Saturn_C-3 comparable Falcon_Heavy.
- Saturn_C-3 countryOrigin United_States.
- Saturn_C-3 diameter "8.128".
- Saturn_C-3 height "81.9912".
- Saturn_C-3 launchSite Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_37.
- Saturn_C-3 launchSite Kennedy_Space_Center.
- Saturn_C-3 manufacturer Boeing.
- Saturn_C-3 manufacturer Douglas_Aircraft_Company.
- Saturn_C-3 manufacturer North_American_Aviation.
- Saturn_C-3 mass "4.64336712E8".
- Saturn_C-3 rocketFunction Low_Earth_orbit.
- Saturn_C-3 rocketFunction Moon.
- Saturn_C-3 rocketStages "3".
- Saturn_C-3 status "Proposed (1961)".
- Saturn_C-3 successor Saturn_INT-20.
- Saturn_C-3 successor Saturn_INT-21.
- Saturn_C-3 wikiPageExternalLink 19740072519_1974072519.pdf..
- Saturn_C-3 wikiPageExternalLink 19790076768_1979076768.pdf..
- Saturn_C-3 wikiPageExternalLink satvint.pdf.
- Saturn_C-3 wikiPageID "11083533".
- Saturn_C-3 wikiPageRevisionID "606106500".
- Saturn_C-3 caption "Saturn C-3B versions, with a nuclear upper stage derivative, 1961".
- Saturn_C-3 comparable Delta_IV_Heavy.
- Saturn_C-3 comparable Falcon_Heavy.
- Saturn_C-3 countryOrigin United_States.
- Saturn_C-3 cpl "43500000".
- Saturn_C-3 cplYear "1985".
- Saturn_C-3 derivatives Saturn_INT-20.
- Saturn_C-3 derivatives Saturn_INT-21.
- Saturn_C-3 family Saturn_(rocket_family).
- Saturn_C-3 function "LEO and Lunar launch vehicle".
- Saturn_C-3 hasPhotoCollection Saturn_C-3.
- Saturn_C-3 manufacturer Boeing.
- Saturn_C-3 manufacturer North_American_Aviation.
- Saturn_C-3 manufacturer "Douglas".
- Saturn_C-3 name "Saturn C-3".
- Saturn_C-3 sites "planned SLC 37, Kennedy Space Center".
- Saturn_C-3 stages "3".
- Saturn_C-3 status "Proposed".
- Saturn_C-3 subject Category:Apollo_program.
- Saturn_C-3 subject Category:Cancelled_space_launch_vehicles.
- Saturn_C-3 subject Category:Saturn_(rocket_family).
- Saturn_C-3 type MeanOfTransportation.
- Saturn_C-3 type Rocket.
- Saturn_C-3 type DesignedArtifact.
- Saturn_C-3 comment "The Saturn C-3 was the third rocket in the Saturn C series studied from 1959 to 1962. The design was for a three-stage launch vehicle that could launch 45,000 kg (100,000 lb) to low Earth orbit and send 18,000 kg (39,000 lb) to the Moon via Trans-Lunar Injection.President Kennedy's proposal on May 25, 1961 of an explicit manned lunar landing goal spurred NASA to concretize its launch vehicle requirements for a lunar landing.".
- Saturn_C-3 label "Saturn C-3".
- Saturn_C-3 label "Saturn C-3".
- Saturn_C-3 label "Saturno C-3".
- Saturn_C-3 sameAs Saturno_C-3.
- Saturn_C-3 sameAs Saturn_C-3.
- Saturn_C-3 sameAs m.02q_g1_.
- Saturn_C-3 sameAs Q3950832.
- Saturn_C-3 sameAs Q3950832.
- Saturn_C-3 wasDerivedFrom Saturn_C-3?oldid=606106500.
- Saturn_C-3 isPrimaryTopicOf Saturn_C-3.
- Saturn_C-3 name "Saturn C-3".