Study of integral launch and reentry vehicle system. Volume 2 - Technology development requirements Final report
Technology development requirements of integral launch and reentry vehicle for space logistics - Vol. 2
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Study of Integral Launch and Reentry Vehicle System. Volume 3: Technical Report - Second Phase: Environment and Performance - Volume III
Environment and performance of integral launch and reentry vehicle for space logistics - Vol. 3
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Study of integral launch and reentry vehicle system. Volume 4 - Technical report Phase 2 - Design and subsystems analysis Final report
Design and subsystems analysis of integral launch and reentry vehicles for space logistics - Vol. 4
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Study of Integral Launch and Reentry Vehicle System. Volume 5 - Technical Report, Phase 2 - Operations and Resources Final Report
Technology and resources for development of integral launch and reentry vehicles for space logistics - Vol. 5
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Pan American World Airways - Present and future plans
Logistics of feeding Boeing 707 and 747 aircraft passengers
Treadwell, J. P.↗
Antarctic research and lunar exploration
Lunar exploration program based on U.S. antarctic research experience, considering man role, environment, logistics, transportation, economics, etc
Johnson, R. W.↗
A space shuttle design consideration
Logistic support reusable earth to orbit space shuttle design, noting weight penalties, payloads and development time
Peterson, C. B.↗
Space Station requirements analysis and preliminary design
Space station requirements and design, discussing space shuttles, operational personnel, long term effects, logistical systems, functions, etc
Brooksbank, W. A., Jr.↗
The Utilization of Halo Orbits in Advanced Lunar Operations
Halo Orbit Space Station potential for lunar communications, exploration, logistics, and launching platform operations
Farquhar, R. W.↗
Development and use of a 12-man space station
NASA orbital space station program, logistics, experimental design, modules and space mission
Dorrenbacher, C. J.↗
Lunar base synthesis study. Volume 2 - Mission analysis and lunar base synthesis Final report
Semipermanent lunar base synthesis, scientific and exploration activities, logistics, and mission analysis
Carpenter, R. B., Jr.↗
MSFC-DPD-235/DR no. SE-07, phase B Mass property status report
Mass properties of space station and logistic module
Kasulka, D. A.↗
Space shuttle operations, maintenance and technology integration
Space shuttle operations, maintenance, and integration of ground support system, logistics, checkout, and recovery
Gay, C. C., Jr.↗
Some considerations in the selection of aircraft for earth resource observations
Comparison of logistics problems and cost aspects in selection of aircraft for earth resources surveys
Arno, R. D.↗
Encapsulated adhesive systems and their potential applications
Microencapsulation of bonded reactive resins in packaging, logistics and adhesive applications at room and elevated temperatures
Davis, T. R.↗
Safety inputs to development program plans
Safety engineers integration into overall system through basic development programs, involving management, manufacturing, testing and integrated logistic support
Ball, L. W.↗
A guide to onboard checkout. Volume 7: RF communications
The radio frequency communications subsystem for a space station is considered, with respect to onboard checkout requirements. The subsystem comprises all equipment necessary for transmitting and receiving, tracking and ranging, command, multiple voice and television information, and broadband experiment data. The communications subsystem provides a radio frequency interface between the space station and ground stations, either directly or indirectly, through a data relay satellite system, independent free-flying experiment modules, and logistics vehicles. Reliability, maintenance, and failure analyses are discussed, and computer programming techniques are presented.
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Experiment module concepts study. Volume 1: Management summary
The minimum number of standardized (common) module concepts that will satisfy the experiment program for manned space stations at least cost is investigated. The module interfaces with other elements such as the space shuttle, ground stations, and the experiments themselves are defined. The total experiment module program resource and test requirements are also considered. The minimum number of common module concepts that will satisfy the program at least cost is found to be three, plus a propulsion slice and certain experiment-peculiar integration hardware. The experiment modules rely on the space station for operational, maintenance, and logistic support. They are compatible with both expendable and shuttle launch vehicles, and with servicing by shuttle, tug, or directly from the space station. A total experiment module program cost of approximately $2319M under the study assumptions is indicated. This total is made up of $838M for experiment module development and production, $806M for experiment equipment, and $675M for interface hardware, experiment integration, launch and flight operations, and program management and support.
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