Browse Items (14 total)
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"Test Laboratory progress report" Febuary and March.
Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March -
"Test Laboratory progress report" May and June.
Monthly rogress report for the test laboratory regarding the Saturn 1B program between Feburary and March -
"Saturn vehicles for Apollo photograph."
8 x 10 inch black and white photograph. Contains images of the Saturn V, Saturn IB and Saturn I in reference to one another -
"Saturn V derivatives."
This paper desciibes an evolutionary family concept of !h turn V derivative launch vehicle systems, discusses their performance capabilities, and outlines their ability to perform orbital and hlgh-energy missions at minimum total program cost. -
"Saturn V quarterly progress report : January - March."
Quarterly progress report for the months of January - March, 1966. -
"Saturn V interface management."
The purpose of the Saturn V Interface Management System is to establish and maintain interface design compatibility between interfacing items under the design responsibility of different agencies. It provides the management tools for effective change control over the design of designated systems and equipment that have critical interface design requirements. -
"Saturn V semi-annual progress report July - December, 1967."
This Saturn V Semi-Annual Progress Report describes progress and major achievements from July 1, 1967 in the Saturn V Program. -
"Apollo 4 press kit."
The flrst flight test of the Apollo/Saturn V space vehicle is scheduled for launch from the Natlonal Aeronautics and Space Administration's John F, Kennedy Space Center, Fla., no earlier than Nov. 7. The mission is designated Apollo 4. -
"Extensions of Saturn."
This paper discusses the possible applications of Saturn vehicles to future space exploration. Potential missions utilizing Apollo derived hardware are examined. Research, development, and operations in earth orbit as well as lunar exploration, unmanned and manned interplanetary exploration are reviewed. These hypothetical missions are discussed in the context of the present and potential capability of three configurations of the Saturn vehicle; an uprated Saturn I, a three-stage Saturn V and a four-stage Saturn V. NOTE: Work presented herein was conducted by the Douglas Missiles and Space Systems Division under company-sponsored research and development funds. Therefore, the concepts and objectives described within this paper reflect the opinions of the authors and do not necessarily constitute endorsement by NASA, the Air Force, or any other U.S. Government organization. The nominal performance numbers presented are typical of the current configurations and possible future vehicle configurations.