NAS 1.21:3078
|
Tables for supersonic flow of helium around right circular cones at zero angle of attack / |
1 |
NAS 1.21:3079
|
Nondestructive evaluation technique guide / |
1 |
NAS 1.21:3080
|
Handbook of infrared radiation from combustion gases / |
1 |
NAS 1.21:3081
|
Auroral bremsstrahlung at balloon altitudes / |
1 |
NAS 1.21:3082
|
Revised tables of airspeed, altitude, and Mach number presented in the international system of units / |
1 |
NAS 1.21:3083
|
ASRDI oxygen technology survey. |
1 |
NAS 1.21:3084
|
ASRDI oxygen technology survey. |
1 |
NAS 1.21:3085/976/
|
Table and charts of equilibrium normal-shock properties for hydrogen-helium mixtures with velocities to 70 km/sec / |
1 |
NAS 1.21:3086
|
Near-infrared spectra of Jupiter, Saturn, and Uranus / |
1 |
NAS 1.21:3087
|
Table and charts of equilibrium normal-shock properties for pure hydrogen with velocities to 70 km/sec / |
1 |
NAS 1.21:3088
|
Thermodynamic and related properties of parahydrogen from the triple point to 300 K at pressures to 1000 bar / |
1 |
NAS 1.21:3089
|
Hydrogen technological survey--thermophysical properties / |
1 |
NAS 1.21:3090
|
ASRDI oxygen technology survey. |
1 |
NAS 1.21:3091
|
Synoptic analyses, 5-, 2-, and O.4-millibar surfaces for January 1972 through June 1973 : a joint NASA-NOAA publication prepared for NASA Wallops Flight Center by the staff, Upper Air Branch, National Weather Service, Camp Springs, Maryland under Wallops Flight Center purchase order number P-55946(G) |
1 |
NAS 1.21:3092
|
ASRDI oxygen technology survey. |
1 |
NAS 1.21:3093
|
Normal- and oblique-shock flow parameters in equilibrium air : including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral / |
1 |
NAS 1.21:3094
|
Spacecraft materials guide / |
1 |
NAS 1.21:3095
|
Diurnal experiment data report, March 19-20, 1974 / |
1 |
NAS 1.21:3096
|
Molecular physics of equilibrium gases : a handbook for engineers / |
1 |
NAS 1.21:3097
|
Tables and charts of equilibrium thermodynamic properties of carbon dioxide for temperatures from 100K to 25,000K / |
1 |