Rocket motor nozzle assembly comprising a refractory metal shell
A Standard patent application filed on 19 January 2001 credited to Shigley, John K. ; Canfield, Alan R.

Details

Application number :

2001252880  

Application type :

Standard  

Application status :

LAPSED  

Under opposition :

No  

Proceeding type :

 

Invention title :

Rocket motor nozzle assembly comprising a refractory metal shell  

Inventor :

Shigley, John K. ; Canfield, Alan R.  

Agent name :

 

Address for service :

 

Filing date :

19 January 2001  

Associated companies :

 

Applicant name :

Alliant Techsystems Inc.  

Applicant address :

 

Old name :

 

Original Source :

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