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Design of a refueling tanker delivering liquid hydrogenA refueling tanker that could deliver 155,000 lb of liquid hydrogen to a hypersonic tanker in 15 min was designed. A flying boom system was chosen to fit strict delivery criteria. Tank design and material specification were also addressed. To assure the flow required, it was important to cancel the pressure drop phenomenon. Geometry, aerodynamics, weight considerations, propulsion, stability, and performance for the tanker were also considered. Finally, the cost of developing three prototypes was estimated.
Document ID
19940021224
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lourme, Daniel
(Ecole Polytechnique Feminine Sceaux, France)
Barnier, Caroline
(Ecole Polytechnique Feminine Sceaux, France)
Faure, Sabine
(Ecole Polytechnique Feminine Sceaux, France)
Pompei, Marie-Helene
(Ecole Polytechnique Feminine Sceaux, France)
Pruniaux, Karine
(Ecole Polytechnique Feminine Sceaux, France)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: USRA, Proceedings of the 8th Annual Summer Conference: NASA(USRA Advanced Design Program
Subject Category
Aircraft Design, Testing And Performance
Accession Number
94N25717
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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