NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The variable density aircraft conceptIn the variable density aircraft concept the aircraft's density is varied by varying its volume. This is accomplished by combining a variable volume hull, which is called the dynapod, with intrinsic means for the controlled variation of a mass of working fluid or substance within the aircraft. The dynapod is a hinged structure and follows the volumetric variations of the working fluid. The result is a variable density hull, which with the attachment of power plants, etc., becomes a variable density aircraft.
Document ID
19760007968
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davenport, A. C.
(Dynapods, Inc. New Orleans, LA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: MIT Proc. of the Interagency Workshop on Lighter than Air Vehicles
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N15056
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available