Gas cooling system for hypersonic vehicle nosetip

Details Gas cooling system for hypersonic vehicle nosetip Gas cooling system for hypersonic vehicle nosetip

1975-04-14

1977-03-29

Blix, Trygve M.

Aeronautics and astronautics

Aircraft structure

102105, 244163, B64C 138

Patent

active

040144852

ABSTRACT:
A cooled nosetip arrangement for a vehicle designed to travel at hypersonic velocities is taught herein. We provide a nosetip having one or more orifices at its forwardmost location, but instead of utilizing an arrangement for expelling a liquid coolant, which would necessitate a considerable amount of plumbing and tankage, we utilize a novel gas generator arrangement enabling a coolant gas to be selectively generated and then expelled from such nosetip orifice(s). In this manner we utilize a coolant that advantageously remains in a chemical form until it is to be actually utilized.

REFERENCES:
patent: 3028129 (1962-04-01), Faillie
patent: 3253405 (1966-05-01), Kropa
patent: 3267857 (1966-08-01), Lindberg, Jr.
patent: 3277825 (1966-10-01), Maillard
patent: 3410502 (1968-11-01), Leadon et al.
patent: 3754511 (1973-08-01), Damon et al.
patent: 3785591 (1974-01-01), Stalmach, Jr.

Affiliated with

Also associated with

Rating

Gas cooling system for hypersonic vehicle nosetip does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas cooling system for hypersonic vehicle nosetip, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas cooling system for hypersonic vehicle nosetip will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-545424