TYPICAL CITATION AND ABSTRACT FROM STAR NASA SPONSORED NASA ACCESSION NUMBER TITLE CONTRACT REPORT N74-28344*# National Aeronautics and Space Administration. SYSTEM SAFETY CHECKLIST SKYLAB PROGRAM RE- Earl M. McNail 30 May 1974 75 p Prepared in cooperation (Contract NAS8-24000) (NASA-TM-X-64850) Avail: NTIS HC $3.75 CSCL 13L Design criteria statement applicable to a wide variety of AVAILABLE ON CORPORATE PUBLICATION DATE AVAILABILITY TYPICAL CITATION AND ABSTRACT FROM /AA NASA SPONSORED AVAILABLE ON AIAA AUTHOR'S CONTRACT GRANT Configuration management during transition Presented in this paper are the analytical and moving-base TYPICAL CITATION AND ABSTRACT FROM STAR NASA SPONSORED NASA ACCESSION NUMBER TITLE CONTRACT REPORT N74-28344*# National Aeronautics and Space Administration. SYSTEM SAFETY CHECKLIST SKYLAB PROGRAM RE- Earl M. McNail 30 May 1974 75 p Prepared in cooperation (NASA-TM-X-64850) Avail: NTIS HC $3.75 CSCL 13L Design criteria statement applicable to a wide variety of flight systems, experiments and other payloads, associated ground support equipment and facility support systems are presented. The document reflects a composite of experience gained throughout the aerospace industry prior to Skylab and additional experience gained during the Skylab Program. It has been prepared to provide current and future program organizations with a broad source of safety-related design criteria and to suggest methods for systematic and progressive application of the criteria beginning with preliminary development of design requirements and specifications. Recognizing the users obligation to shape the checklist to his particular needs, a summary of the historical background, rationale, objectives, development and implementation approach, and benefits based on Skylab experience has been included. Author AVAILABLE ON CORPORATE PUBLICATION DATE AVAILABILITY TYPICAL CITATION AND ABSTRACT FROM IAA NASA SPONSORED AVAILABLE ON AIAA AUTHOR'S AFFILIATION CONTRACT OR A74-37834 * # Configuration management during transition for a powered lift STOL aircraft. W. A. Johnson and S. J. Craig (Systems Technology, Inc., Hawthorne, Calif.). American Institute of Aeronautics and Astronautics, Mechanics and Control of Flight Conference, Anaheim, Calif., Aug. 5-9, 1974, Paper 74-836. 6 p. 5 refs. Members, $1.50; nonmembers, $2.00. Contract No. NAS26441. Presented in this paper are the analytical and moving-base simulation results of a study to improve flight safety and operations of V/STOL type aircraft. One of the more significant and novel aspects of the work accomplished has been the concept and implementation of a configuration management flight control system designed to take the guesswork out of, and improve the operational safety of, transition flight in the region from cruise to STOL. |