NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Tethered orbital refueling studyObjectives are to evaluate the feasibility and limitations of fluid acquisition and transfer under an accleration induced in a tethered orbital refueling facility and to provide conceptual designs. Program tasks consist of recommendation of fluid transfer method and parameters; evaluation of disturbances, fluid motion, and damping; selection of passive devices to augment inherent fluid damping and determination of the resultant envelope of operation; assessment of the effect of tether lengths on hazards; and identification of ground and flight tests necessary to prove the tethered orbital refueling concepts.
Document ID
19860018175
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fester, D. A.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Publication Information
Publication: NASA, Washington Applications of Tethers in Space: Workshop Proceedings, Vol. 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86N27647
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

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