Ordnance – Rocket launching – Method of making
Patent
1997-06-24
1998-11-17
Jordan, Charles
Ordnance
Rocket launching
Method of making
89 1816, 89 1809, F41F 304
Patent
active
058379177
ABSTRACT:
A cooling system for a missile launcher having a plurality of missile-containing cells connected to a common plenum. Disposed in the plenum beneath each missile is an impingement plate in the path of hot exhaust gas from the missile. A cooling water injection nozzle is arranged below each impingement plate and is supplied with cooling water during a hot missile launch to cool the hot exhaust gas and the plenum.
REFERENCES:
patent: 3182554 (1965-05-01), Barakauskas
patent: 3499364 (1970-03-01), D'Ooge
patent: 3516380 (1970-06-01), Johnston
patent: 4373420 (1983-02-01), Piesik
patent: 4436016 (1984-03-01), Olmsted et al.
patent: 4686884 (1987-08-01), Piesik
patent: 5162605 (1992-11-01), Piesik
patent: 5191162 (1993-03-01), Czimmek
patent: 5375502 (1994-12-01), Bitsakis
Macnab Donald A.
Wei James P.
Jordan Charles
Northrop Grumman Corporation
Sutcliff Walter G.
Wesson Theresa M.
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