NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Probe samples components of rocket engine exhaustWater-cooled, cantilevered probe samples the exhaust plume of rocket engines to recover particles for examination. The probe withstands the stresses of a rocket exhaust plume environment for a sufficient period to obtain a useful sample of the exhaust components.
Document ID
19650000381
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Schumacher, P. E.
Date Acquired
August 2, 2013
Publication Date
December 1, 1965
Subject Category
Materials
Report/Patent Number
MFS-485
Report Number: MFS-485
Accession Number
65B10384
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available