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Film script for Saturn C-1/C-1B quarterly film report no. 13 (covering July, August, September, 1962).
Film script reporting on how the Saturn 1 will be used and what its take-off process will look like -
Script for Saturn C-1/C-1B quarterly film report no. 14 (covering Oct., Nov., Dec., 1962).
Film script reporting on how the Saturn 1 will be used and what its take-off process will look like -
"Technological problems of the Saturn class vehicle."
Aerospace Workshop. University of Hawaii.; Includes references to slides. -
Saturn V news reference.
This book is designed to serve as an aid to newsmen in present and future coverage of the Saturn IB in its role in the Saturn/Apollo Program and as a general purpose large launch vehicle. -
"Saturn V space program and aluminum welding technology."
This paper discusses the flaws and limitations with welding technology, specifically with the techniques involved. -
"Saturn base heating review."
The Saturn I booster which is powered by a cluster of eight rocket engines has been successfully flown on four successive flights. The early success of this large launch vehicle is a strong indication of the soundness of its base heating program. This paper summarizes the thinking that went into the design of our base configuration. Flight test results indicate that pressures, temperatures and heating rates were generally as expected. New techniques have been investigated for generating design data. It has been found experimentally that pressure and thermal fields establish themselves in one to three milliseconds and that data from the "short duration" technique compare favorably with "long duration" type tests. As a result, the new "short duration" technique has become the standard for generating design data for the Saturn vehicle. -
"Saturn IB SA-217 reference launch vehicle."
This document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical-mile circular orbit is 44,965 pounds. The Saturn IB SA-217 launch vehicle is to be used as the baseline vehicle for advanced studies requiring the use of the standard or modified Saturn IB launch vehicle. This vehicle definition does not necessarily represent approved changes to any specific vehicle. This document supersedes the Saturn IB SA-213 reference Launch Vehicle, described in memorandum R-P&VE-DIR-65-92. -
"Saturn S-IVB quarterly technical progress report."
Douglas Aircraft Company Report DAC-56445, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during August and September 1966. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-101. -
"S-IVB Saturn high energy upper stage and its development."
The development of carrier rockets For manned space missions has been one of the major activities in the aerospace field during the past decade. The early space efforts were made possible by the existence of large ballistics missiles. It soon became obvious that the delivery of weapons and the launch of large spacecraft could not be combined into one operational system in an efficient way; therefore, a family of spacecraft boosters had to be created. -
"Saturn S-IVB quarterly technical progress report."
Douglas Aircraft Company Report DAC-56533, Saturn S-IVB Quarterly Technical Progress Report, covers design and development progress on the Saturn IB and Saturn V configurations of the S-IVB stage during January, February, and March 1967. This report is prepared for the National Aeronautics and Space Administration under Contract NAS7-01.; Prepared for National Aeronautics and Space Administration under NASA contract NAS7-101.; Approved by A. P. O'Neal, Director, Saturn Development Engineering.