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.
Testing Microgravity Flight Hardware Concepts on the NASA KC-135
39th Aerospace Sciences Meeting ; 2001 ; Reno, NV, United States
01.03.2001
Preprint
Keine Angabe
Englisch