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  • 1
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    STS-9 BET products (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The final products generated for the STS-9, which landed on December 8, 1983 are reported. The trajectory reconstruction utilized an anchor epoch of GMT corresponding to an initial altitude of h 356 kft, selected in view of the limited tracking coverage available. The final state utilized IMU2 measurements and was based on processing radar tracking from six C-bands and a single S-band station, plus six photo-theodolite cameras in the vicinity of Runway 17 at Edwards Air Force Base. The final atmosphere (FLAIR9/UN=581199C) was based on a composite of the remote measured data and the 1978 Air Force Reference Atmosphere model. The Extended BET is available as STS9BET/UN=274885C. The AEROBET and MMLE input files created are discussed. Plots of the more relevant parameters from the AEROBET (reel number NL0624) are included. Input parameters, final residual plots, a trajectory listing, and data archival information are defined.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-172314 , NAS 1.26:172314 , AMA-84-3
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Final STS-11 (41-B) best estimate trajectory products: Development and results from the first Cape landing (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The STS-11 (41-B) postflight data processing is completed and the results published. The final reconstructed entry trajectory is presented. The various atmospheric sources available for this flight are discussed. Aerodynamic Best Estimate of Trajectory BET generation and plots from this file are presented. A definition of the major maneuvers effected is given. Physical constants, including spacecraft mass properties; final residuals from the reconstruction process; trajectory parameter listings; and an archival section are included.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-172349 , NAS 1.26:172349 , AMA-84-4
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    The definition of the Shuttle Tethered Aerothermodynamic Research Facility (1985)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Studies have been conducted to define the feasibility and practical limitations of the Shuttle Orbiter Tethered 'wind-tunnel' concept. This concept, referred to as the Shuttle Tethered Aerothermodynamic Research Facility (STARFAC), is proposed to provide researchers access to altitudes above 90 km to accomplish aerothermodynamic research in the rarefied upper atmosphere. Determining the feasibility and limitations of the concept has required the enhancement and/or development of mission simulation analytical techniques and control laws; the accomplishment of candidate mission simulations; the definition of instrumentation requirements, both for science and engineering; and the establishment of tether and satellite design requirements to meet STARFAC objectives. The results of the study, to date, indicate that such a concept is both feasible and practical. Representative results are presented, as are recommendations for continued studies which would result in program implementation.
    Keywords: SPACE TRANSPORTATION
    Type: AIAA PAPER 85-1794
    Format: text
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    NASA TECHNICAL REPORTS
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