This test was conducted to verify that A/A44A-1A Rocket Motors with carbon nozzle inserts, purposely damaged beyond specification limits, could be utilized in the operational inventory without creating a 'safety of flight' hazard. A secondary test requirement was to determine if an adequate method could be devised to repair the damaged areas. (Author)
Serviceability Test of a/A44-1A Rocket Motors with Damaged Nozzle Inserts (Air-2A Rocket)
1968
23 pages
Report
No indication
English
Rocket Engines & Motors , Missile Technology , Air to air missiles , Nozzle inserts , Rocket nozzles , Performance(Engineering) , Guided missile safety , Exhaust nozzles , Graphite , Rocket igniters , Captive tests , Damage assessment , Machining , Epoxy resins , Value engineering , Reliability , Air force logistics command , Genie
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