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  • 1995-1999  (1)
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    Controls concepts for next generation reuseable rocket engines (1995)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Three primary issues will drive the design and control used in next generation reuseable rocket engines. In addition to steady-state and dynamic performance, the requirements for increased durability, reliability and operability (with faults) will dictate which new controls and design technologies and features will be brought to bear. An array of concepts which have been brought forward will be tested against the measures of cost and benefit as reflected in the above 'ilities'. This paper examines some of the new concepts and looks for metrics to judge their value.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: NASA-TM-106902 , E-9594 , NAS 1.15:106902 , 1995 American Control Conference; Jun 21, 1995 - Jun 23, 1995; Seattle, WA; United States
    Format: application/pdf
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