NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Development of a rocketborne spectroradiometer to measure the radiation environment of a reentry vehicle.Rocketborne spectroradiometer measurement of spectral radiation intensity of luminescent air in shock induced flow field produced by reentry vehicle
Document ID
19640038667
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Husson, C.
Spiers, R. B., Jr.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Machine Elements And Processes
Report/Patent Number
AIAA PAPER 63-376
Report Number: AIAA PAPER 63-376
Accession Number
64A24560
Distribution Limits
Public
Copyright
Other
Keywords
SHOCK SPECTRUM
FLOW FIELD
RADIOMETER
REENTRY EFFECT
ROCKET MEASUREMENT

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19640038679Collected WorksPhysico-chemical diagnostics of plasmas, american institute of aeronautics and astronautics, and northwestern university, gas dynamics laboratory, biennial symposium, 5th, proceedings.
No Preview Available