The radiator/heat exchanger set-up shows how the radiation problem was ultimately solved. The engineers placed a small SNAP-8 sized reactor in the middle of a reactor and cooled it with molten metal and circulated it through the heat exchanger.
The SNAP-8 could easily fit inside the J-58 engine of the Blackbird.
The autoignition temperatures for JP-7 depending on the atmospheric conditions range from 900K to 1050K or in fahrenheit 1160F to 1430F [1]. So, if what we know about JP-7 from open sources is true, then it was developed to autoignite at altitude when exposed to the 900-1050 Kelvin temperature of the air coming from the radiator.
This was a test of the radiator of the liquid core aircraft reactor. |
1. https://www.researchgate.net/publication/268480192_Development_of_a_Detailed_Chemical_Kinetic_Mechanism_for_Combustion_of_JP-7_Fuel
Development of a Detailed Chemical Kinetic Mechanism for Combustion of JP-7 Fuel
July 2003
DOI: 10.2514/6.2003-4939
Conference: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Authors:
Tae Park
Mohammed A Mawid
14.78Engineering Research & Analysis Co
Balu Sekar
Carlos Arana
VERY INFORMATIVE ARTICLE. Thanks
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