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TYPICAL CITATION AND ABSTRACT FROM STAR

NASA SPONSORED
DOCUMENT

NASA

ACCESSION NUMBER

TITLE

CONTRACT
OR GRANT

REPORT
NUMBER

N74-28344*# National Aeronautics and Space Administration.
Marshall Space Flight Center, Huntsville, Ala.

SYSTEM SAFETY CHECKLIST SKYLAB PROGRAM RE-
PORT

Earl M. McNail 30 May 1974 75 p Prepared in cooperation
with Martin Marietta Aerospace, Denver

(Contract NAS8-24000)

(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 implementa-
tion approach, and benefits based on Skylab experience has
been included.
Author

AVAILABLE ON
MICROFICHE

CORPORATE
SOURCE

PUBLICATION

DATE

AVAILABILITY
SOURCE

TYPICAL CITATION AND ABSTRACT FROM /AA

NASA SPONSORED
DOCUMENT

AVAILABLE ON
MICROFICHE

AIAA
ACCESSION
NUMBER

AUTHOR'S
AFFILIATION

CONTRACT
OR

GRANT

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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. NAS2-
6441.

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.

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TYPICAL CITATION AND ABSTRACT FROM STAR

NASA SPONSORED
DOCUMENT

NASA

ACCESSION NUMBER

TITLE

CONTRACT
OR GRANT

REPORT
NUMBER

N74-28344*# National Aeronautics and Space Administration.
Marshall Space Flight Center, Huntsville, Ala.

SYSTEM SAFETY CHECKLIST SKYLAB PROGRAM RE-
PORT

Earl M. McNail 30 May 1974 75 p Prepared in cooperation
with Martin Marietta Aerospace. Denver
(Contract NAS8-24000)

(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
MICROFICHE

CORPORATE
SOURCE

PUBLICATION

DATE

AVAILABILITY
-SOURCE

TYPICAL CITATION AND ABSTRACT FROM IAA

NASA SPONSORED
DOCUMENT

AVAILABLE ON
MICROFICHE

AIAA
ACCESSION
NUMBER

AUTHOR'S AFFILIATION

CONTRACT

OR
GRANT

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.

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