MEDICAL AND BIOLOGICAL ASPECTS OF THE ENERGIES OF SPACE. ENERGY - THE KEY TO SPACE EXPLORATION
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Ostrander, D. R.↗
SEARCH · Engineering Papers
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Address by dr. george e. mueller, associate administrator for manned space flight, national aeronautics and space administration, at the dedication of the magic mountain laboratory of the marquardt corporation, van nuys, california, october 30, 1964
Objectives of nasa program and apollo project contribution - dedication speech
APOLLO PROJECT↗
The origin and evaluation of atmospheres and oceans, proceedings of a conference, nasa, goddard space flight center, goddard institute for space studies, new york, n.y., april 8, 9, 1963.
Conference on origin and evolution of atmospheres and oceans at New York City in April 1963
PLANETARY ATMOSPHERE↗
Space structures space technology project no. 8
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Chaput, A. J.↗
Space materials handbook. Supplement 1 to the second edition - Space materials experience Technical report, Oct. 1964 - Sep. 1965
Spacecraft structures and systems materials handbook
HANDBOOK↗
National Aeronautics and Space Administration Space Cell Test Program Monthly progress report, 1-30 Sep. 1966
Life cycle tests conducted with nickel-cadmium, siver-cadmium, and silver-zinc cell packs as part of NASA program
NICKEL-CADMIUM BATTERY↗
Goddard 1965 - A Year in Review at Goddard Space Flight Center National Aeronautics and Space Administration
Chronological data on satellite launchings and accomplishments of 1965
HISTORY↗
Analysis and design of space vehicle flight control systems. Volume XII - Attitude control in space
Analysis and design of attitude control systems for earth orbiting satellite
SYSTEMS DESIGN↗
Research and advanced development. Volume I. Supporting research and technology for the Office of Space Sciences and Applications, National Aeronautics and Space Administration Semiannual review, 1 Jan. - 30 Jun. 1967
Research and technology review in fields of lunar and planetary exploration, physics, astronomy, and bioscience
PLANETARY EXPLORATION↗
Space programs summary no. 37-33, volume 3 for the period march 1, 1965 to april 30, 1965. the deep space network
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Relevance of a space-research centrifuge to future space-flight programs.
Centrifuge on board orbiting spacecraft as research tool for biological and physical experiments relevant to prolonged missions and spacecraft design
Newsom, B. D.↗
National Aeronautics and Space Administration space cell test program Monthly progress report, Oct. 1969
Performance tests of spacecraft cells
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Contributions of the Space Programme to Aviation: Space and Aviation: Lecture 13 - Session E
Application of spacecraft technology to aircraft for improvement in systems, materials, and performance
Cohen, H.↗
Space shuttle: Effects of horizontal tail geometry and position on longitudinal stability of model S-5, NASA/MSC 0.01875 space orbiter shuttle
Low speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
Pope, H. A.↗
Space shuttle: Aerodynamic heating to the Grumman space shuttle orbiters (ROS-NB1 and ROS-WB1) at Mach number 8.0
Hypersonic wind tunnel test of two delta wing orbiter models
D'Errico, A.↗
Space Shuttle: Static pressure distribution on Chrysler Corporation Space Division SERV booster configuration
A dual purpose test was conducted in the propulsion wind tunnel (PWT) to evaluate the performance of an aerospike engine, in the presence of a booster, and obtain forebody and base pressure distributions on the booster in which it is installed. The test item was a 2.5 percent scaled replica of the SERV booster employing a 5 percent spike length aerospike engine installed in the base region of the model. Cold flow air was used to simulate engine jet operation. Two booster configurations were investigated, one on which reentry aerospike engine thermal protection doors were installed, and another where the doors were removed. The data presented are representative of the latter configuration for a Mach number range of 0 to 1.25 at angles of attack of 0 and 8 degrees and 0 degrees angle of sideslip.
Price, E. A.↗
Development of a space stable thermal control coatings for use in large space vehicles
The preparation and evaluation of zinc orthotitanate and of several new pigments and the environmental testing and evaluation of these pigments and of coatings made from them constitute the bulk of the work accomplished. New pigments were prepared and EPR spectra of pigments and their precursor compounds studied. Results of extensive testing of commercially-available, strippable, protective coatings are reported; Owens-Illinois 650 glass resin has been stabilized against progressive mechanical failures; and definite improvements have been noted. A zinc oxide pigmented lithium silicate paint has demonstrated very good ultraviolet stability.
Gilligan, J. E.↗
Methodologies for optimal resource allocation to the national space program and new space utilizations. Volume 2: Resource allocation and smoothing model, programmer's manual
Appendixes are presented that provide model input requirements, a sample case, flow charts, and a program listing. At the beginning of each appendix, descriptive details and technical comments are provided to indicate any special instructions applicable to the use of that appendix. In addition, the program listing includes comment cards that state the purpose of each subroutine in the complete program and describe operations performed within that subroutine. The input requirements includes details on the many options that adapt the program to the specific needs of the analyst for a particular problem.
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