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  • PROPULSION SYSTEMS  (1,456)
  • 1970-1974  (1,456)
Collection
Keywords
Years
Year
  • 1
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    Design of Liquid Propellant Rocket Engines Second Edition (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines and systems
    Keywords: PROPULSION SYSTEMS
    Type: NASA-SP-125
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Launching of SERT 2 (1970)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: In-orbit performance tests of ion engines and exhaust effects on SERT 2 equipment
    Keywords: PROPULSION SYSTEMS
    Type: NASA-NEWS-RELEASE-70-8
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 3
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    Turbofan engine for shuttle (1970)
    In:  CASI
    Details
    Publication Date: 2019-08-27
    Description: Air breathing engines for space shuttle reentry
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-66716
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 4
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    Liquid rocket pressure regulators, relief valves, check valves, burst disks, and explosive valves (1973)
    In:  CASI
    Details
    Publication Date: 2019-08-27
    Description: The development of and operational programs for effective use in design are presented for liquid rocket pressure regulators, relief valves, check valves, burst disks, and explosive valves. A review of the total design problem is presented, and design elements are identified which are involved in successful design. Current technology pertaining to these elements is also described. Design criteria are presented which state what rule or standard must be imposed on each essential design element to assure successful design. These criteria serve as a checklist of rules for a project manager to use in guiding a design or in assessing its adequacy. Recommended practices are included which state how to satisfy each of the criteria.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-SP-8080
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 5
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    Solid Rocket Motor Performance Analysis and Prediction (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-27
    Description: Current design practices are reviewed and assessed, and guidance is established for achieving greater consistency in design, reliability in the end product, and efficiency in the design effort. The total problem is discussed, and design elements involved in successful design are identified. Design criteria are described, and the rule, guide, limitation, or standard which must be imposed on each essential design element is given. Recommended practices are presented for satisfying each of the criteria.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-SP-8039
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 6
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    On the Design and Test of a Liquid Injection Electric Thruster (1973)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: A liquid injection electric thruster (LINJET) was designed and tested. The results of the tests were very encouraging with thruster performance levels well in excess of design goals. Supporting activities to the engine design and test included a five-million pulse life test on the main capacitor, a 46-million pulse test on the trigger electronics, design and fabrication of a zero resistance torque connector for use with the torsional pendulum thrust stand, design and fabrication of a logic box for control of engine firing, and a physical and chemical properties characterization of the perfluorocarbon propellant. While the results were encouraging, testing was limited, as many problems existed with the design. The most significant problem was involved with excessive propellant flow which contributed to false triggering and shorting. Low power active thermal control of the propellant storage cavity, coupled with a re-evaluation of the injection ring pore size and area exposed to the main capacitor discharge are areas that should be investigated should this design be carried forward.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-132316
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 7
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    Advanced injector concepts investigation Final summary report (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: Evaluation of throttling injector concepts applicable to advanced cryogenic engines
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-103183 , REPT-21052-3FS
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 8
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    NASA aircraft engine noise research. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: NASA research and development work on the noise of aircraft engines suitable for use on conventional take-off and landing subsonic cruise airplanes is reviewed. The work discussed was part of the NASA Quiet Engine program. Salient results in the areas of fan, jet and complete propulsion system noise are presented and briefly discussed.
    Keywords: PROPULSION SYSTEMS
    Type: ICAS PAPER 72-48 , International Council of the Aeronautical Sciences, Congress; Aug. 28, 1972-Sept. 2, 1972; Amsterdam; Netherlands
    Format: text
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    NASA TECHNICAL REPORTS
  • 9
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    NASA overview of electric propulsion. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: The current NASA technology program aimed at auxiliary and primary electric propulsion is summarized. The early application of this technology continues to be a major goal of the program. The status and objectives of the presently planned flight experiments and the future technology goals in auxiliary electric propulsion are reviewed. Progress and direction of on-going programs for developing the technology of solar electirc primary propulsion are also presented.
    Keywords: PROPULSION SYSTEMS
    Type: AIAA PAPER 72-1127 , Joint Propulsion Specialist Conference; Nov 29, 1972 - Dec 01, 1972; New Orleans, LA; US
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 10
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    NASA's quiet engine programs. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: It is the goal of NASA to provide the technology that will make the aircraft unobtrusive in its environment. The primary work in propulsion source noise reduction centers around the technology to modify existing engines and the technology to design new propulsion systems for CTOL, STOL, and VTOL that operate at significantly lower noise levels than present systems. It is recommended that noise standards should also be established for new engines. Another recommendation is concerned with the incorporation of noise and pollution technology in military aircraft propulsion developments.
    Keywords: PROPULSION SYSTEMS
    Type: Journal of Air Traffic Control; 14; Sept
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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