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Performance of a UTC FW-4S solid propellant rocket motor under the command effects of simulated altitude and rotational spin [PDF]

One United Technology Center FW-4S solid-propellant rocket motor was fired at an average simulated altitude of 103,000 ft while spinning about its axial centerline at 180 rpm. The objectives of the test program were to determine motor altitude ballistic
Merryman, H. L., Smith, L. R.
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RSRM-3 (360L003) Ballistics/Mass Properties Report [PDF]

The propulsion performance and reconstructed mass properties data from Morton Thiokol's RSRM-3 motors which were assigned to the STS-29 launch are presented. The composite type solid propellant burn rates were close to predicted.
Laubacher, B. A., Richards, M. C.
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An inventory of aeronautical ground research facilities. Volume 1: Wind tunnels [PDF]

A survey of wind tunnel research facilities in the United States is presented. The inventory includes all subsonic, transonic, and hypersonic wind tunnels operated by governmental and private organizations.
Brown, K. R. +3 more
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Solid rocket technology advancements for space tug and IUS applications [PDF]

In order for the shuttle tug or interim upper stage (IUS) to capture all the missions in the current mission model for the tug and the IUS, an auxiliary or kick stage, using a solid propellant rocket motor, is required.
Ascher, W., Bailey, R. L., Behm, J. W., Gin, W. +3 more
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Pathophysiology of free-bullet slaughter of horses and ponies [PDF]