columbus · Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration

Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration

Title: Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Incomplete
Report Number: RTD TDR 63-4179 Part 1
Corporate Author: Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: AF Flight Dynamics Laboratory
Extent: 167
Identifier: AD0433097
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(616)-8130
DoD Project: 8219
DoD Task: 821902
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available by request
Date Issued: 1964-02
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA; Lockheed Martin Missiles & Fire Control
Type: report
Creator: Kaufman, Louis G., II