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Development of the NASA ZPS Mark III 57.2-kN/m2 (8.3 psi) Space Suit NASA Lyndon B. Johnson Space Center

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kosmo, Joseph J., author.
Conference Name:
Intersociety Conference on Environmental Systems (1988-07-11 : San Francisco, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1988
Summary:
The NASA-developed space-suit configurations for Project Mercury and the Gemini Program originated from high-altitude-aircraft full-pressure-suit technology. These early suits lacked sophisticated mobility systems, since the suit served primarily as a backup system against the loss of cabin pressure and required limited pressurized intravehicular mobility functions for a return capability. Beginning with the Gemini Program, enhanced mobility systems were developed to enable crewmembers to perform useful tasks outside the spacecraft. The zero-prebreathe Hark III (ZPS Mk III) model of a higher operating pressure (57.2 kN/m2 (8.3 psi)) space-suit assembly represents a significant phase in the evolutionary development of a candidate operational space-suit system for the Space Station Program. The various design features and planned testing activities for the ZPS Mk III 57.2-kN/m2 (8.3 psi) space suit are described and identified
Notes:
Vendor supplied data
Publisher Number:
881101
Access Restriction:
Restricted for use by site license

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