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NASA NTRS · 20010051293

Testing Microgravity Flight Hardware Concepts on the NASA KC-135

Abstract

This paper provides an overview of utilizing the NASA KC-135 Reduced Gravity Aircraft for the Foam Optics and Mechanics (FOAM) microgravity flight project. The FOAM science requirements are summarized, and the KC-135 test-rig used to test hardware concepts designed to meet the requirements are described. Preliminary results regarding foam dispensing, foam/surface slip tests, and dynamic light scattering data are discussed in support of the flight hardware development for the FOAM experiment.

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BibTeXRIS

Motil, Susan M., Harrivel, Angela R., Zimmerli, Gregory A.. 2001-03-01. Testing Microgravity Flight Hardware Concepts on the NASA KC-135. https://ntrs.nasa.gov/citations/20010051293

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