LOOK AT NASA's REVIEW >>>>>>>>
An e-mail from the evaluator of the
THRUST concept dated July 30, 2001 in part states;
"Your proposal for the THRUST concept will operate. There is some
engineering needed to get the optimum diameter (for proper power frequency,
g-loads on the engines, stresses, etc), the design of the thrust deflector
plates, the actual heat exchanger design, actual inlet ducting design.etc"
This statement emerged following a six month evaluation