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  • 1
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    Optimized space shuttle trajectory simulation (1972)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A computer program for simulating optimized space shuttle trajectories is presented. The program considers the ascent, return, and synergetic maneuvers of lifting boosters and spacecraft. Other constraints on optimum trajectory such as maximum heating, acceleration, angle of attack, and excluded or included overflight or impact regions are examined. Mathematical models are included to support the theoretical aspects of the discussion.
    Keywords: SPACE SCIENCES
    Type: NASA. Langley Res. Center Space Shuttle Aerothermodyn. Tech. Conf., vol. 4; p 1439-1473
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Low-thrust, minimum-fuel, orbital transfers (1971)
    In:  Other Sources
    Details
    Publication Date: 2019-06-27
    Description: Low thrust minimum fuel space vehicle transfer from initial circular orbit to coplanar elliptic orbit of given energy and angular momentum
    Keywords: SPACE SCIENCES
    Type: ; ADEMIE DES SCIENCES
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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