Operation and Service Manual for ECS Coolant System Leak Rate Tester 52E180150.

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Abstract:

The purpose of this report is to familiarize personnel with the operation and service instructions for the ECS Coolant System Leak Rate Tester, 52E180150-153. The leak rate tester provides the capability to leak check the coolant system pump module prior to installation into the Gemini B Spacecraft and the entire spacecraft coolant system after installation into the spacecraft. This report presents a description of the leak rate tester, its control panel and associated equipment, and service instructions for preventive maintenance. Author

Author(s):
No Author(s) Identified
Author Organization(s):
MCDONNELL DOUGLAS ASTRONAUTICS CO ST LOUIS MO
Pagination:
0028

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
B5-10-27
Contract/Grant Number(s):
F04695-67-C-0023
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_6.4_Information Assurance; JCA_6_Net Centric
Communities of Interest:
Space
Descriptor(s):
*MANNED SPACECRAFT, CONTROLLED ATMOSPHERES, CONTROLLED ATMOSPHERES, LEAK DETECTORS, PNEUMATIC EQUIPMENT, PRESSURIZATION, FIRE SAFETY, MAINTENANCE, CALIBRATION
Field(s)/Group(s):
Ground Support Systems and Facilities for Space Vehicles, Manned Spacecraft
Keyword(s):
ECS(ENVIRONMENTAL CONTROL SYSTEM), ENVIRONMENTAL CONTROL SYSTEM, GEMINI, *GEMINI B PROJECT, *MANNED ORBITING LABORATORIES, *MOL(MANNED ORBITING LABORATORIES)
Report Date:
1969 Feb 03