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{ "item_title" : "Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment", "item_author" : [" Jeremy S. Goodwin "], "item_description" : "This research effort builds upon the previous design of the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX). RIGEX is a Space Shuttle experiment that will study the effects of the zero-gravity space environment on the deployment and modal analysis of three in-atable and rigidizable tubes using a sub-Tg rigidizationtechnique. By comparing space-based modal testing with similar ground-based tests, the experiment intends to verify and validate ground-testing techniques as a viablesubstitute for zero-gravity tests, thus minimizing cost and complexity for future AirForce and commercial spacecraft rigidization implementations.With the transition from the Space Shuttle's Get-Away-Special (GAS) canisterto its Canister for All Payload Ejections (CAPE) in 2004, there have been severalrequirements and associated modi cations a ecting the design", "item_img_path" : "https://covers2.booksamillion.com/covers/bam/1/28/833/264/1288332645_b.jpg", "price_data" : { "retail_price" : "18.95", "online_price" : "18.95", "our_price" : "18.95", "club_price" : "18.95", "savings_pct" : "0", "savings_amt" : "0.00", "club_savings_pct" : "0", "club_savings_amt" : "0.00", "discount_pct" : "10", "store_price" : "" } }
Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment|Jeremy S. Goodwin

Detailed Design of the Rigidizable Inflatable Get-Away-Special Experiment

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Overview

This research effort builds upon the previous design of the Rigidizable Inflatable Get-Away-Special Experiment (RIGEX). RIGEX is a Space Shuttle experiment that will study the effects of the zero-gravity space environment on the deployment and modal analysis of three in-atable and rigidizable tubes using a sub-Tg rigidizationtechnique. By comparing space-based modal testing with similar ground-based tests, the experiment intends to verify and validate ground-testing techniques as a viablesubstitute for zero-gravity tests, thus minimizing cost and complexity for future AirForce and commercial spacecraft rigidization implementations.With the transition from the Space Shuttle's Get-Away-Special (GAS) canisterto its Canister for All Payload Ejections (CAPE) in 2004, there have been severalrequirements and associated modi cations a ecting the design

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Details

  • ISBN-13: 9781288332649
  • ISBN-10: 1288332645
  • Publisher: Biblioscholar
  • Publish Date: November 2012
  • Dimensions: 9.21 x 6.14 x 0.41 inches
  • Shipping Weight: 0.61 pounds
  • Page Count: 192

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