Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields - Info and Reading Options
By Kalinski, Michael E.
"Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields" and the language of the book is English.
“Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields” Metadata:
- Title: ➤ Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields
- Author: Kalinski, Michael E.
- Language: English
“Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields” Subjects and Themes:
- Subjects: ➤ Space stations - Space debris - orbital debris - hyper-velocity impact - International Space Station - Whipple Shield - Enhanced Stuffed Whipple Shield - NASA - ballistic limit equations
Edition Identifiers:
- Internet Archive ID: hypervelocityimp109451233
AI-generated Review of “Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields”:
"Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields" Description:
The Internet Archive:
The International Space Station (ISS) must be able to withstand the hypervelocity impacts of micrometeoroids and orbital debris that strike its many surfaces. In order to design and implement shielding which will prevent hull penetration or other operational losses, NASA must first model the orbital debris and micrometeoroid environment. Based upon this environment, special multi-stage shields called Whipple and Enhanced Stuffed Whipple Shields are developed and implemented to protect ISS surfaces. Ballistic limit curves that establish shield failure criteria are determined via ground testing. These curves are functions of material strength, shield spacing, projectile size, shape and density, as well as a number of other variables. The combination of debris model and ballistic limit equations allows NASA to model risk to ISS using a hydro-code called BUMPER. This thesis modifies and refines existing ballistic limit equations for U.S. Laboratory Module shields to account for the effects of projectile (debris/ micro-meteoroid) densities. Using these refined ballistic limit equations this thesis also examines alternative shielding materials and configurations to optimize shield design for minimum mass and maximum stopping potential, proposing alternate shield designs for future NASA ground testing. A final goal of this thesis is to provide the Department of Defense a background in satellite shield theory and design in order to improve protection against micrometeoroid and orbital debris impacts on future spacebased national systems.
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"Hypervelocity Impact Analysis Of International Space Station Whipple And Enhanced Stuffed Whipple Shields" is available for download from The Internet Archive in "texts" format, the size of the file-s is: 795.53 Mbs, and the file-s went public at Fri May 03 2019.
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