-40%

Lot of NASA Technical Notes D-1231 to D-1249 1962 Apollo, Gemini Era-See Details

$ 44.88

Availability: 100 in stock

Description

Lot of 16 NASA Technical Note D-1231 to D-1249 1962 Apollo, Gemini Era
All in very good condition!
From a library collection of more than 1,000 NASA Technical Notes. Final picture is of complete collection.
Details of this lot:
D-1231
Mar-62
A Rigidly Forced Oscillation System For Measuring Dynamic-Stability Parameters in Transonic and Supersonic Wind Tunnels
D-1232
Apr-62
Static Aerodynamic Characteristics of a Two-Stage and a Three-Stage Rocket Vehicle At Mach Numbers From 1.47 to 4.63
D-1233
Mar-62
Effects of Coupling Between Pitch and Roll Control Inputs of the Handling Qualities of VTOL Aircraft
D-1234
Apr-62
Force-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellors
D-1235
Apr-62
Flight-Test Investigation of a Model of an Aerial Vehicle Supported by Four Unshrouded Propellors
D-1236
Apr-62
Experimental Investigation of Oscillatory Aerodynamic Forces, Moments, and Pressures Acting on a Tapered Wing Oscillating in Pitch at Mach Numbers from 0.40 to 1.07
D-1238
Mar-62
Experimental Observations of Aerodynamic and Heating Tests on Insulating Heat Shields
D-1239
May-62
An Experimental Study of the Effect of Downwash From A Twin-Propellor VTOL Aircraft on Several Types of Ground Surfaces
D-1241
Apr-62
Effects of Suction Boundary-Layer Control on the Performance of a Short Annular Diffuser with an Upstream Terminal Normal Shock
D-1242
May-62
Theoretical Investigation of Effects of Changes in Command Computations and Filter Location on Response of an Automatically Controlled Interceptor During the Attack Phase
D-1243
Apr-62
Design of the NASA Lightweight Inflatable Satellites for the Determination of Atmospheric Density at Extreme Altitudes
D-1244
Apr-62
A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having The Same Planform But Different Surface Shapes
D-1246
Apr-62
Pressure Measurements on Two 60° Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0° and 45° At a Mach Number of 4.95
D-1247
Apr-62
A Matrix Method For the Determination of the Natural Vibrations of Free-Free Unsymmetrical Beams with Application to Launch Vehicles
D-1248
May-62
The Meteoric Hazard of the Environments of a Satellite
D-1249
Jul-62
Statistical Wind Distribution Data For Use At NASA Wallops Station