3 edition of Space shuttle flying qualities and criteria assessment found in the catalog.
Space shuttle flying qualities and criteria assessment
by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va
Written in English
|Statement||T.T. Myers, D.E. Johnston and D.T. McRuer.|
|Series||NASA contractor report -- 4049., NASA contractor report -- NASA CR-4049.|
|Contributions||Johnston, Donald E., McRuer, Duane T., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.|
|The Physical Object|
Subsonic cruise mode for intact abort during ascent phase of space shuttle vehicles. Read more. Article. Space shuttle flying qualities criteria assessment, phase 3 Orbiter Flying Qualities. 6 Longitudinal Criteria 11 Long-Period Flying Qualities Criteria (MIL-FC) •Static speed stability –No tendency for aperiodic divergence •Phugoid oscillation -> 2 real roots, 1 that is unstable –Stable control stick position and force gradients •e.g., Increasing pull position and force with decreasing speed A. Non-terminal flight requiring rapid.
prior to flying the Space Shuttle again. Another 14 recommendations from the Board are being implemented as well by NASA. Additionally, the agency has gone above and beyond the CAIB recommendations with a list of 15 corrective actions known as “Raising the Bar” to make the Space Shuttle safer than it has ever been. Space science pioneer - James Van Allen, key contributor to 25 space missions. Engineers draw the cutting edge in every capacity for NASA, from avionics to electronics, software to rocketry. Similarly, to explain the things and places it explores, NASA enlists scientists from a multitude of specialties within the fields of astronomy, biology.
The space shuttle orbiter has already been struck many times by small meteoroids and orbital debris, but it has not been damaged severely. There is a real risk, however, that a meteoroid or debris impact could one day force the crew to abort a mission or might result in loss of life or loss of the shuttle itself. The Approach and Landing Tests were a series of taxi and flight trials of the prototype Space Shuttle Enterprise, conducted in to test the vehicle's flight characteristics both on its own and when mated to the Shuttle Carrier Aircraft, prior to the operational debut of the Shuttle system.
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Space Shuttle Flying Qualities Criteria Assessment Phase IV Data Acquisition and Analysis T. Myers, D. Johnston,and D. McRuer Systems Technology, Inc., South Hawthorne Boulevard, Hawthorne, California Prepared for Ames Research Center Dryden Flight Research Facility Edwards, California Contract NAS2 NI\SI\.
Space shuttle flying qualities and criteria assessment. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Branch, March (OCoLC) Material Type: Government publication, National government publication: Document Type: Book: All Authors / Contributors.
Get this from a library. Space Shuttle flying qualities criteria assessment--phase III. [Thomas T Myers; Donald E Johnston; Duane T McRuer; Systems Technology, Inc.,; Dryden Flight Research Facility,; United States.
National Aeronautics and Space Administration,]. Space Shuttle Flying Qualities and Criteria Assessment T. Myers, D. Johnston, and D. McRuer Systems Technology, Inc.
Hawthorne, California Prepared for Ames Research Center Dryden Flight Research Facility under Contract NAS NASA National Aeronautics and Space Administration Scientific and Technical Information Branch Space shuttle flying qualities and criteria assessment. By T. Myers, Duane T.
Mcruer and D. Johnston. and preparation of an OEX approach to produce a data archive and optimize use of the data to develop flying qualities for future space shuttle craft in general. Analytic modeling of the Orbiter's unconventional closed-loop dynamics. Space Shuttle flying qualities and flight control system assessment.
By T. Myers, Questions arising from this examination are addressed through comparisons with MIL-FC and other proposed flying qualities criteria which indicate potential longitudinal flying qualities problems. However, it is shown that these criteria, based largely.
A program of flying qualities experiments as part of the Orbiter Experiments Program (OEX) is defined. Phase 1, published as CR, reviewed flying qualities criteria and shuttle data. The review of applicable experimental and shuttle data to further define the OEX plan is continued.
Space Shuttle Flying Qualities and:Flight ~Control System Assessment Stu«:ly --Phase II Flight IControl System Assessment Stu~dy--Phase T.
Myers, D. Johnston, and D. McRuer Configurations Compared to Exemplary Criteria 29 (TS 2 = sec). Space shuttle flying qualities and criteria assessment study--phase 11 [microform] / T.T.
Myers, D.E. Jo Space shuttle flying qualities criteria assessment phase IV [microform]: data acquisition and analysis The space shuttle at work / Howard Allaway; Space shuttle glider [electronic resource]. Flying qualities from early airplanes to the Space Shuttle.
William H. Phillips ; William H. Phillips. NASA Langley Research Center, Hampton, Virginia. Search for more papers by this author Some Results In Flying Qualities Criteria Developed at PVL.
Space Shuttle longitudinal landing flying qualities. Bruce G. Powers ; Bruce G. Powers. Space Shuttle Landing and Rollout Training at the Vertical Motion Simulator. Steven Beard, Unified flying qualities criteria for longitudinal tracking.
WILSON. The suitability of existing and proposed flying quality and flight control system criteria for application to the space shuttle orbiter during atmospheric flight phases was assessed. An orbiter experiment for flying qualities and flight control system design criteria is discussed.
NAS and NAS, Space Shuttle Flying Qualities and Flight Con trol System Criteria Assessment, Phases I and II. It provides continu ation and refinement of a program for the Orbiter Experimental Program (OEX) titled Flying Qualities and Flight Control Systems Design Criteria Experiment (OFQ). Space shuttle, partially reusable rocket-launched vehicle designed to go into orbit around Earth, to transport people and cargo to and from orbiting spacecraft, and to glide to a runway landing on its return to Earth’s surface.
It was developed by NASA and made spaceflights between and Space shuttle flying qualities and criteria assessment. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.]: [For sale by the National Technical Information Service], (OCoLC) Material Type.
FLYING QUALITIES CRITERIA FOR SUPERAUGMENTED AIRCRAFT Donald T. Berry NASA Ames Research Center Space Shuttle, AFTVF-I6 and X=29 BIBLIOGRAPHY Flying Qualities and Flight Control Assessment Study,' Phase 1, NASA CR. Get this from a library. Space shuttle flying qualities criteria assessment phase IV: data acquisition and analysis.
[Thomas T Myers; Donald E Johnston; Duane T McRuer; Ames Research Center.; Dryden Flight Research Facility.; Systems Technology, Inc.]. handling qualities development and the use of the Cooper-Harper pilot rating scale is presented as background for spacecraft handling qualities research, development, test, and evaluation (RDT&E).
In addition, handling qualities experiences and lessons-learned from previous United States (US) spacecraft developments are reviewed. This report is. The Space Shuttle was a partially reusable low Earth orbital spacecraft system that was operated from to by the National Aeronautics and Space Administration (NASA) as part of the Space Shuttle official program name was Space Transportation System (STS), taken from a plan for a system of reusable spacecraft of which it was the only item funded for development.
American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA. Static stability was not required since the design criteria allowed reliance on the flight control system to meet flying qualities criteria.
Early simulations Identified a flight control requirement for static longitudinal stability to be no more than two percent body length ( percent mean aerodynamic chord) unstable so the pitching.Assessment of flying-quality criteria for air-breathing aerospacecraft.
By Donald E. Johnston, Duane T. Mcruer, Experience with the space shuttle orbiter is reviewed with respect to flight control system mechanization and flight experience in approach and landing flying qualities .American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA