Lot of 19 NASA Technical Notes D-1720 to D-1739 Apollo, Gemini Era-See Detail

Description

Lot of 19 NASA Technical Notes D-1720 to D-1739 Apollo, Gemini Era Research
All complete and in great condition!
Details of contents:
D-1720
May-63
Electron-Hydrogen Phase Shifts Just Below the Inelastic Threshold
D-1721
May-63
The Effect of Refraction on the Setting Sun as Seen From Space in Theory and Observation
D-1722
Apr-63
Results of Mocrometeorite Penetration Experiment on the Explorer VII Satellite (1959 IOTA)
D-1723
Feb-63
Lunar Landing Propulsion Considerations
D-1724
Feb-63
Calibrations and Comparisons of Pressure-Type Airspeed-Altitude Systems of the X-15 Airplane from Subsonic to High Supersonic Speeds
D-1725
Aug-63
Techniques Used to Measure the Hydraulic Characteristics of the NASA Plum Brook Reactor
D-1726
Jun-63
Experimental Investigation of Rocket-Engine Ablative Material Performance After Postrun Cooling at Altitude Pressures
D-1727
Jun-63
Experimental Evaluation of Liquid-Fluorine System Components
D-1728
May-63
Rate of Liquid Jet Breakup By a Transverse Shock Wave
D-1729
Jun-63
Calibration of a Thermal-Conductivity Vacuum Gage in the Range of 10^-4 to 1 Torr by Means of a Volume-Ratio Calibration System
D-1730
Nov-63
The N-Body Code - A General Fortran Code for the Numerical Solution of Space Mechanics Problems on an IBM 7090 Computer
D-1731
Jul-63
Leak-Rate Testing of the NASA Plum Brook Reactor Containment Vessel
D-1732
Jun-63
Possible Effects of Nonuniform Flows on Performance of Electrothermal Thrustors
D-1733
Jul-63
Nautralizer Tests on a Flight-Model Electron-Bombardment Ion Thruster
D-1734
Jun-63
Dispersion and Damping of Longitudinal Electron Oscillations in Thermal Plasmas
D-1735
Sep-63
Table of OF
2
F1 (a,b;c;z) For a=0(1/2)7, b=0(1/2)7, and c=0(1/2)5/2 with Comments on Closed Forms of OF2F1 (a,b;c;z)
D-1737
Oct-63
A General IBM 704 or 7090 Computer Program for Computation of Chemical Equilibrium Compositions, Rocket Performance, and Chapman-Jouguet Detonations
D-1738
Nov-63
Effects of Regenerative and Radiation Cooling on Performance of Electrothermal Thrustors
D-1739
Aug-63
Compatibility of Cesium Vapor with Selected Materials at Temperature to 1200℉