Hello all,
I am working on implementing a NASA design from 68 into my project for orbiter. The report contained HERE has some really good details but lacks the critical Neon system schematic.
I managed to diagram the system based on the description:
I didn't include it in the diagram but I am going to assume the Ne Inlet temp is 2000R since that is the temp in the report for the Ne periphery. so it has to release about 13000R into the H2, "Cold" Ne and the centrifuge. Additionally 0.19lb/sec is calculated as the Ur bleed off from the core which accounts for 800Btu/sec.
What I would like to know:
Based on the above information is there a way to calculate the temperatures at each heat exchanger with a similar style as shown in Fig 8 on P77 of the NASA report? If so, how would I calculate it?
Thanks!
I am working on implementing a NASA design from 68 into my project for orbiter. The report contained HERE has some really good details but lacks the critical Neon system schematic.
I managed to diagram the system based on the description:
I didn't include it in the diagram but I am going to assume the Ne Inlet temp is 2000R since that is the temp in the report for the Ne periphery. so it has to release about 13000R into the H2, "Cold" Ne and the centrifuge. Additionally 0.19lb/sec is calculated as the Ur bleed off from the core which accounts for 800Btu/sec.
What I would like to know:
Based on the above information is there a way to calculate the temperatures at each heat exchanger with a similar style as shown in Fig 8 on P77 of the NASA report? If so, how would I calculate it?
Thanks!