AS8581: Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust - Technical Standard

Features

Issuing Committee: Aerospace Council

Scope

Content: This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.

Meta Tags

Topics: Rocket engines
Solid propellants
Environmental testing
Quality control
Fire fighting
Assembling
Test procedures
Test equipment and instrumentation
Ignition systems

Details

DOI: https://doi.org/10.4271/AS8581

Pages: 19

Citation: SAE International Technical Standard, Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust, SAE Standard AS8581, Issued March 2000, https://doi.org/10.4271/AS8581.

Additional Details

Publisher: SAE International

Published: Mar 1, 2000

Product Code: AS8581

Content Type: Technical Standard

Status: Issued

Language: English