Accession Number:

ADD002282

Title:

Rocket Motor Apparatus.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s):

• Panella,Edward A.

Report Date:

1975-11-18

Pagination or Media Count:

5.0

Abstract:

The patent relates to a method whereby a plurality of perforated tubes are placed longitudinally between the insulator layer and silicone rubber layer of a stress relieving rocket motor liner to insure proper pressure distribution within the motor during burn.

Descriptors:

• *Solid propellant rocket engines
• *Rocket propellant grains
• *Pressure distribution
• *Patents
• Combustion
• Stress relieving
• Combustion chamber liners

Subject Categories:

• Solid Propellant Rocket Engines
• Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE