NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A summary of the CHARGE-2 electron beam rocket experimentThe major purpose of the CHARGE-2 experiment was to study the interaction of a vehicle at high potential (up to 1 kV) with the ionosphere. The payload consisted of two parts that were separated during the flight. The high potential was obtained by electron emission from the mother vehicle, and by voltage-biasing of the daughter vehicle. Measurements of transient vehicle potential were obtained with a sample internal of 100 ns. The mother current collection exhibited magnetic limitations above 240 km. Below 240 km the mother collected a current far in excess of the magnetically limited models. This demonstrates the ability of an electron beam to interact with the neutral atmosphere at altitudes below 240 km.
Document ID
19900051640
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, Neil B.
(USAF, Rome Air Development Center Hanscom AFB, MA, United States)
Raitt, W. John
(Utah State University Logan, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 90-1554
Accession Number
90A38695
Funding Number(s)
CONTRACT_GRANT: NAGW-235
CONTRACT_GRANT: NAG5-607
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available