columbus · Force Balance Determination of Inlet Performance for Advanced Vehicle Applications to Orbital Velocities Using Internal Drag Measurements

Force Balance Determination of Inlet Performance for Advanced Vehicle Applications to Orbital Velocities Using Internal Drag Measurements

Title: Force Balance Determination of Inlet Performance for Advanced Vehicle Applications to Orbital Velocities Using Internal Drag Measurements
Date: 1963
Index Abstract: Coming Soon
Photo Quality: Incomplete
Report Number: ASD TDR 63-701
Corporate Author: Aeronautical Systems Division
Laboratory: Aeronautical Systems Division
Extent: 23
Identifier: AD0426728
Access Rights: OTS
Distribution Classification: 1
Contract: None Given
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1963-09
Abstract: The abstract for this report is either unavailable or has yet to be entered
Type: report
Provenance: Lockheed Martin Missiles & Fire Control
Format: 23 pages ; 28 cm.
Creator: Kutschenreuter, Paul H., Jr.