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SECTION IBIOMEDICAL RESULTS OF APOLLO
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لينك | نوشته شده در 87/08/19ساعت 11:35 توسط rahmang |
EXTRAVEHICULAR MOBILITY UNIT

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Introduction

The Apollo extravehicular mobility unit was designed to meet a unique set of needs. To assure the maximum return of scientific information from the moon, a method was required for collecting samples, deploying/retrieving instruments, and performing experiments on the lunar surface and in free space. Man had to be able to operate safely in free space to provide an emergency mode of translation from the Lunar Module to the Command Module in the event a complete linkup could not be accomplished after lunar lift-off. Since the weight required to provide redundant pressure vessels for each spacecraft would have been prohibitive, a space suit was required

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The extravehicular mobility unit (EMU) design reflected these needs. Figure 1 is a cutaway representation of the EMU. The unit consisted of a highly mobile, anthropomorphic pressure vessel and a portable life support system (PLSS). The pressure vessel, known as the pressure garment assembly (PGA), when operated in conjunction with the Command Module and Lunar Module life support systems, provided pressurization backup during critical mission phases, including launch and return. It provided primary pressurization for the extravehicular activity conducted from the Command Module during the missions of Apollo 15, 16, and 17. Traverses of four to seven hours’ duration were made with the PLSS on the lunar surface to perform the lunar science tasks.

A description of the EMU used for the first lunar landing is given here. A short description is included of the changes made in the EMU design during the program to incorporate the results of experience and to provide new capabilities.

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The EMU was supplied by three different concerns. The pressure garment assembly was supplied by ILC Industries, Incorporated, and the portable life support system by the Hamilton Standard Division of United Aircraft Corporation. Both were under the monitorship of the Crew SYstems Division of the Engineering and Development Directorate of the Johnson Space Center. The communications equipment was supplied by RCA under the monitorship of the Tracking and Communications Development Division, also of the Engineering and Development Directorate.


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لينك | نوشته شده در 87/08/13ساعت 8:36 توسط rahmang |