Invention Grant
- Patent Title: Low velocity injector manifold for hypergolic rocket engine
- Patent Title (中): 低压喷射器歧管用于高压火箭发动机
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Application No.: US12193679Application Date: 2008-08-18
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Publication No.: US09404441B2Publication Date: 2016-08-02
- Inventor: William S. Brown , Thomas M. Walczuk , Rodney Noble , Frederick Dodd
- Applicant: William S. Brown , Thomas M. Walczuk , Rodney Noble , Frederick Dodd
- Applicant Address: US CA Canoga Park
- Assignee: AEROJET ROCKETDYNE OF DE, INC.
- Current Assignee: AEROJET ROCKETDYNE OF DE, INC.
- Current Assignee Address: US CA Canoga Park
- Agent Joel G Landau
- Main IPC: F02K9/52
- IPC: F02K9/52 ; F02K9/44
Abstract:
A fuel manifold for a thrust chamber assembly includes a main fuel chamber which is generally frustro-conical in shape. The main fuel chamber provides a resonance frequency that is different than an acoustic resonance frequency of a combustion chamber.
Public/Granted literature
- US20100037590A1 LOW VELOCITY INJECTOR MANIFOLD FOR HYPERGOLIC ROCKET ENGINE Public/Granted day:2010-02-18
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