NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Structural Certification of Human-Rated Inflatable Space StructuresThis paper details the results of an initial study to develop a certification plan for human-rated inflatable space structures, including guidelines for qualification testing. Habitable softgoods inflatables are multi-layered shell structures that use high-strength webbing, cordage and broadcloth fabric to carry the skin loads of a variety of volumetric shapes and structural architectures. The primary objectives of this study are to define the key parameters that affect these structures and propose a statistically robust approach to defining safety and knockdown factors based on test and analysis. Current NASA standards for habitable inflatable space structures use a factor of safety of 4, which was inherited from airship design criteria. An updated approach to defining a design factor, taking into account material strength variability, load variability in the article, number of test samples, and damage and degradation effects is specified. Accurate analytical modeling of these structures is hindered by the difficulty of obtaining accurate and consistent material data due to load-history- dependent, nonlinear load versus strain behavior. A building block approach to certification is detailed that uses stochastic modeling and statistical test design and analysis to address the unique challenges these high-strength softgoods structures present. Human-rated inflatable modules are a transformative capability for launching much larger habitable volumes into space than is possible with rigid shell structures. This research aims to provide the framework for certifying these structures for future human space exploration missions.
Document ID
20180006204
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jones, Thomas C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 9, 2018
Publication Date
March 3, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-27608
Report Number: NF1676L-27608
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 3, 2018
End Date: March 10, 2018
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: WBS 089407.01.23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available