Accession Number : AD0856737
Title : MOL Fluid Dynamics Preliminary Data Report: Thrustor Plume Tests. Sequence Number B319. Item Data Number UT-132,
Corporate Author : MCDONNELL DOUGLAS ASTRONAUTICS CO-HB HUNTINGTON BEACH CA
Personal Author(s) : Lofland, M. L.
Report Date : 10 MAR 1969
Pagination or Media Count : 123
Abstract : An experimental test program was conducted to assess the effects of rocket exhaust plume impingement on MOL vehicle surfaces and equipment. Testing was performed in a vacuum chamber by use of flat panels to represent vehicle surfaces and a subscale thrustor. The program included surface heating tests and exhaust contamination investigations, with emphasis on the latter. Devices and techniques to control thrustor contamination were evaluated. Test data included plume mapping and thermal heating measurements; in situ measurements of thermal radiative and optical properties of selected contamination specimens; laboratory analyses of contamination deposits; and movie and still photographic coverage. (Author)
Descriptors : *NOZZLE GAS FLOW), (*MANNED SPACECRAFT, (*SPACE STATIONS, NOZZLE GAS FLOW), SPACE CAPSULES, EXHAUST GASES, IMPACT, SURFACES, PANELS, THERMAL RADIATION, CONTAMINATION, ROCKET NOZZLES.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE