Call Number (LC) | Title | Results |
---|---|---|
NAS 1.26:182276 | Arcjet thruster research and technology | 1 |
NAS 1.26:182278 | Propfan Test Assessment (PTA) flight test report / | 2 |
NAS 1.26:182279 | Orbit transfer rocket engine technology program integrated control and health monitoring capacitive displacement sensor development : final report / | 1 |
NAS 1.26:182280 | Space station hydrogen/oxygen thruster technology / | 1 |
NAS 1.26:182281 | Finite element modeling of frictionally restrained composite interfaces | 1 |
NAS 1.26:182283 | Plasma contractor research, 1989 annual report / | 1 |
NAS 1.26:182284 | Computed performance of the half-scale accurate antenna reflector | 1 |
NAS 1.26:182285 | Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation | 1 |
NAS 1.26:182286 | Laser velocimeter and total pressure measurements in circular-to-rectangular transition ducts | 1 |
NAS 1.26:182288 | Oscillating flow loss test results in Stirling engine heat exchangers | 1 |
NAS 1.26:182289 | Improved silicon carbide for advanced heat engines | 1 |
NAS 1.26:182290 | Manifest a computer program for 2-D flow modeling in Stirling machines / | 1 |
NAS 1.26:182291 | Theoretical analysis of compatibility of several reinforcement materials with NiAl and FeAl matrices | 1 |
NAS 1.26:182293 |
Droplet sizing instrumentation used for icing research operation, calibrarion, and accuracy / Droplet sizing instrumentation used for icing research operation, calibration, and accuracy / |
2 |
NAS 1.26:182294 |
Reusable rocket engine turbopump health monitoring system, final report, contract NAS3-25279 / Reusable rocket engine turbopump health management system |
2 |
NAS 1.26:182296/ | Shear flow control of cold and heated rectangular jets by mechanical tabs | 1 |
NAS 1.26:182297 | Unsteady stagnation-point heat transfer during passage of a concentrated vortex | 1 |
NAS 1.26:182298 | Time-dependent computational studies of flames in microgravity | 1 |
NAS 1.26:182301 | ||
NAS 1.26:182302 | Stability robustness improvement of direct eigenspace assignment based feedback systems using singular value sensitivities | 2 |