NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Non-Axisymmetric Inflatable Pressure Structure (NAIPS) Concept that Enables Mass Efficient Packageable Pressure Vessels with Sealable OpeningsAchieving minimal launch volume and mass are always important for space missions, especially for deep space manned missions where the costs required to transport mass to the destination are high and volume in the payload shroud is limited. Pressure vessels are used for many purposes in space missions including habitats, airlocks, and tank farms for fuel or processed resources. A lucrative approach to minimize launch volume is to construct the pressure vessels from soft goods so that they can be compactly packaged for launch and then inflated en route or at the final destination. In addition, there is the potential to reduce system mass because the packaged pressure vessels are inherently robust to launch loads and do not need to be modified from their in-service configuration to survive the launch environment. A novel concept is presented herein, in which sealable openings or hatches into the pressure vessels can also be fabricated from soft goods. To accomplish this, the structural shape is designed to have large regions where one principal stress is near zero. The pressure vessel is also required to have an elongated geometry for applications such as airlocks.
Document ID
20160013336
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Doggett, William R.
(NASA Langley Research Center Hampton, VA, United States)
Jones, Thomas C.
(NASA Langley Research Center Hampton, VA, United States)
Kenner, Winfred S.
(NASA Langley Research Center Hampton, VA, United States)
Moore, David F.
(NASA Langley Research Center Hampton, VA, United States)
Watson, Judith J.
(NASA Langley Research Center Hampton, VA, United States)
Warren, Jerry E.
(NASA Langley Research Center Hampton, VA, United States)
Makino, Alberto
(NASA Ames Research Center Moffett Field, CA, United States)
Yount, Bryan
(NASA Ames Research Center Moffett Field, CA, United States)
Selig, Molly
(NASA Johnson Space Center Houston, TX, United States)
Shariff, Khadijah
(NASA Johnson Space Center Houston, TX, United States)
Litteken, Douglas
(NASA Johnson Space Center Houston, TX, United States)
Mikulas, Martin M., Jr.
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
November 9, 2016
Publication Date
August 1, 2016
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-24908
NASA/TM-2016-219331
L-20730
Report Number: NF1676L-24908
Report Number: NASA/TM-2016-219331
Report Number: L-20730
Funding Number(s)
WBS: WBS 432938.11.01.07.43.40.12
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available