Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

APPLICATION OF THE CLOSED-CYCLE PRINCIPLE TO AIRCRAFT PROPULSION SYSTEMS. VOLUME VIII, CHAPTERS 1 TO 9. SIZING OF THE COMPONENTS OF A CLOSED-CYCLE He-NAP SYSTEM. (Cover carries title: CLOSED CYCLE AIRCRAFT PROPULSION SYSTEMS)

Technical Report ·
OSTI ID:4295259
Work on sizing of axial compressor, turbines, fans, recuperator, cooler, ducting, and auxillaries for a hellum closed-cycle nuclear aircraft propulsion system is described. (T.R.H.)
Research Organization:
Escher Wyss GmbH, Zurich
NSA Number:
NSA-13-005157
OSTI ID:
4295259
Report Number(s):
AFOSR-TR-58-32; AD-152241
Country of Publication:
United States
Language:
English