When the space shuttle’s external tank (ET) was being filled with the cryogenic fuel components LOX and LH2, moisture from the surrounding atmosphere could condense onto the ET’s sprayed-on foam insulation (SOFI). This condensation could drip onto components, such as the LOX feed line bellows, where it would freeze, forming a potentially dangerous ice block.
The math model and software were developed in order to assist in the design of an IR heat projection system consisting of halogen light bulbs and parabolic reflectors. Due to pad safety requirements, the system was deployed at a distance of approximately 135 m from the ET surface to be heated.
Features of the software are specifically directed toward the ET SOFI heating application using projected heat lamps. The basic math modeling technique, using Monte Carlo integration and geometric ray tracing, can lead to many other applications in optics as well as acoustics, or anything involving wave energy propagation, with the constraint that waves are incoherent, reflecting surfaces are ideal, and atmospheric attenuation can be neglected.
This work was done by Robert Youngquist of Kennedy Space Center, and Steven Klinko and John Lane of ASRC Aerospace Corporation. U.S. persons may obtain this software at no cost from the Open Channel Foundation website at http://openchannelfoundation.org/projects/Ray_Tracing_Math_Model/ . KSC-12835