Call Number (LC) Title Results
NAS 1.15:4390 Free-volume characteristics of epoxies 1
NAS 1.15:4391 Aerothermal test results from the second flight of the Pegasus® booster 1
NAS 1.15:4392 Functional requirements document for the Earth Observing System Data and Information System (EOSDIS) Scientific Computing Facilities (SCF) of the NASA/MSFC Earth Science and Applications Division, 1992 1
NAS 1.15:4393 Flight-determined benefits of integrated flight-propulsion control systems 1
NAS 1.15:4394 Integrated flight propulsion control research results using the NASA F-15 HIDEC flight research facility 1
NAS 1.15:4395 Indexes of maps of the planets and satellites 1992 1
NAS 1.15:4396 In-flight simulation studies at the NASA Dryden Flight Research Facility 1
NAS 1.15:4397 The mechanical behavior of cross-rolled beryllium sheet 1
NAS 1.15:4398 In-flight leading-edge extension vortex flow-field survey measurements on a F-18 aircraft at high angle of attack 1
NAS 1.15:4400 Subsonic flight test evaluation of a performance seeking control algorithm on an F-15 airplane 1
NAS 1.15:4402 A monitor for the laboratory evaluation of control integrity in digital control systems operating in harsh electromagnetic environments 1
NAS 1.15:4406 Automatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraint 1
NAS 1.15:4407 Total temperature probes for high-temperature hypersonic boundary-layer measurements 1
NAS 1.15:4408 Target fragmentation in radiobiology 1
NAS 1.15:4409 Application of laser doppler velocimeter to chemical vapor laser system 1
NAS 1.15:4410 A study of the generation of linear energy transfer spectra for space radiations 1
NAS 1.15:4411 Computational parametric study of sidewall-compression scramjet inlet performance at mach 10 1
NAS 1.15:4412 Controls-structures interaction guest investigator program overview and phase I experimental results and future plans / 1
NAS 1.15:4413 Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 1
NAS 1.15:4415 Flight test results from a supercritical mission adaptive wing with smooth variable camber 1