Analysis Of Limiting Thermal Conditions Encountered By A Manned Space Suit In Orbit

Item

Title
Analysis Of Limiting Thermal Conditions Encountered By A Manned Space Suit In Orbit
Date
1963
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AMRL TDR 63-102
Creator
Irvine, Thomas F., Jr.
Cramer, Kenneth R.
Corporate Author
State Univ Of New York Stony Brook
Laboratory
Biomedical Laboratory
Extent
26
Identifier
AD0429184
Access Rights
OTS
Distribution Classification
1
Contract
Laboratory Research - No Contract
DoD Project
6301
DoD Task
630104
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Cover Price
0.75
Abstract
In this study, three thermal problems have been examined which occur in the design of space suits to be used when personnel are outside the parent vehicle. The first concerns the time-temperature variation of an infinite thermal conductivity suit exposed to extreme conditions of heating and cooling. The second is related to temperature differences which may occur from the top to the bottom of the suit, thereby causing physiological discomfort. Finally, the scheme was examined whereby these temperature differences might be ameliorated by circulating a fluid in passages behind the suit material.
Report Availability
Full text available
Date Issued
1963-11
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource