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  • 1
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-18
    Description: The Shuttle flight test plan is detailed, together with the results of tests of the flight control system (FCS). The initial Columbia flights carried 13,000 lb of instrumentation, and will be replaced with a 97 lb package during subsequent flights when further data are desired. The flight test program, besides gathering aerodynamic data, was heavily concerned with the perormance of the SSME (near-nominal), the thermal protection system (the performance and reusability have been demonstrated), and the data processing system (ground verification tests vindicated). Ascent has been nominal, as have orbital maneuvers, and descent roll/yaw has proven smoother than other high performance aircraft. Accelerometers and crewmembers have not been able to sense the smoothness of reentry RCS-controlled maneuvers. The manual controls are noted to serve only in off-nominal situations. The STS is concluded to be a basically sound vehicle, assuring a routine American presence in space.
    Keywords: SPACE TRANSPORTATION
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  • 2
    facet.materialart.
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    In:  Other Sources
    Publication Date: 2011-08-17
    Description: The paper discusses the plans for the stability and control aspects of the Space Shuttle orbital flight testing. The first flight plan calls for the design of trajectory, cg, and trim schedules which are as tolerant as possible with regard to all the constraints and aerodynamic uncertainties. Vehicle configuration control and downmoding switches will be used to provide capabilities to handle the off-nominal conditions that might be encountered. Measured trim conditions will provide information on the control effector characteristics and provide an early estimate of the control boundaries.
    Keywords: SPACE TRANSPORTATION
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  • 3
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    In:  Other Sources
    Publication Date: 2011-08-17
    Description: The current plan for a flight test program to support the Skylab revisit and to accommodate changes in the schedule is presented. The stability and control aspects of the entry flight phase are discussed. The orbiter flight control effectors and their characteristics are described. The approach chosen for orbital flight testing was examined.
    Keywords: SPACE TRANSPORTATION
    Type: SETP SETP Tech. Rev., Vol. 14, No. 2; p 11-20
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