Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory
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Report Number: AEDC TN 60-191
Author(s): Gray, J. Don
Corporate Author(s): VKF, ARO, Inc.
Date of Publication: 1960-11
Pages: 36
Contract: AF 40(600)-800
DoD Project: None Given
Identifier: AD0246085
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: IIT
Author(s): Gray, J. Don
Corporate Author(s): VKF, ARO, Inc.
Date of Publication: 1960-11
Pages: 36
Contract: AF 40(600)-800
DoD Project: None Given
Identifier: AD0246085
Abstract:
The abstract for this report is either unavailable or has yet to be entered
Provenance: IIT