SAE International Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust AS8581

Description
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.
  • Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust - AS8581 - SAE International
    SAE International
Description
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.

Suppliers

Company
Product
Description
Supplier Links
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust - AS8581 - SAE International
SAE International
Warrendale, PA, United States
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
AS8581
Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust AS8581
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.

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.

Supplier's Site

Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number AS8581
Product Name Engine; Rocket, Solid Propellant 5 Second Duration, 4500 Pounds Thrust
Unlock Full Specs
to access all available technical data

Similar Products