LOW-COST FABRICATION TECHNIQUES FOR SOLID ROCKET NOZZLES

Format:

Conference/Event

Author/Creator:

WARGA, J. J., author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (1970-10-05 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1970

Summary:

Savings of 50 percent can be achieved in ablative nozzles for 260-inches-dia solid rocket motors using present state-of-the-art materials. An optimum nozzle design with respect to cost and performance results from the use of a standard carbon-phenolic tape grade for the throat insert and canvas, carbon-silica and silica materials throughout the remainder of the nozzle

Notes:

Vendor supplied data

Publisher Number:

700796

Access Restriction:

Restricted for use by site license