Pratt & Whitney aircraft nuclear J-8 turbojet engine performance variation with radiator diameter
- Pratt and Whitney Aircraft, East Hartford, CT (United States)
The variation of engine performance with liquid metal radiator diameter and flight altitude has been estimated for both the 1600F NaK and 1800F NaK radiators at Mach 0.6 and hot day atmospheric conditions. The net thrust, air flow and reactor power is presented in 3 figures for the Pratt & Whitney Aircraft J-58 engine with the 1600F NaK radiator. The net thrust, air flow and reactor power for the 1800F NaK radiator are also presented in figures.
- Research Organization:
- Pratt and Whitney Aircraft, East Hartford, CT (United States)
- Sponsoring Organization:
- US Atomic Energy Commission (AEC)
- DOE Contract Number:
- AC02-84PW02789
- OSTI ID:
- 1245463
- Report Number(s):
- CNLM--2283
- Country of Publication:
- United States
- Language:
- English
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