columbus · Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory

Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory

Title: Drag and Stability Derivatives of Missile Components According to the Modified Newtonian Theory
Date: 1960
Index Abstract: Limited
Photo Quality: Not Needed
Report Number: AEDC TN 60-191
Corporate Author: VKF, ARO, Inc.
Extent: 36
Identifier: AD0246085
Distribution Classification: 2
Contract: AF 40(600)-800
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Not available via Contrails
Date Issued: 1960-11
Abstract: The abstract for this report is either unavailable or has yet to be entered
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Research and Development Command, USAF
Provenance: IIT
Type: report
Creator: Gray, J. Don