Call Number (LC) Title Results
NAS 1.26:183187 Compact imaging spectrometer for induced emissions final technical report / 1
NAS 1.26:183188 Application of acoustic-Doppler current profiler and expendable bathythermograph measurements to the study of the velocity structure and transport of the Gulf Stream 1
NAS 1.26:183189 Multicolor pyrometer for materials processing in space, phase II. 1
NAS 1.26:183191 Program of research in structures and dynamics final report. 1
NAS 1.26:183192 Analysis and modeling of summertime convective cloud and precipitation structure over the southeastern United States semiannual report for the period 15 March to 15 September 1988 / 1
NAS 1.26:183193 Numerical computation of space shuttle orbiter flow field final report, NASA grant NAS 2-245, October 1, 1983 - May 1, 1988. 1
NAS 1.26:183195 An investigation of new methods for estimating parameter sensitivities 1
NAS 1.26:183196 Material growth and characterization for solid state devices final technical report / 1
NAS 1.26:183197 Sensitivity, optimal scaling, and minimum roundoff errors in flexible structure models progress report / 1
NAS 1.26:183198 Final report on shuttle Centaur engine cool down evaluation and effects of expanded inlet on start transient 1
NAS 1.26:183199 RL10 ignition limits test for shuttle Centaur final report / 1
NAS 1.26:183200 RL10A-3-3B high mixture ratio qualification program final report / 1
NAS 1.26:183201 Final report on all shuttle Centaur engine and nozzle support plug vibration testing 1
NAS 1.26:183202 Final technical report on robust design of distributed controllers for large flexible space structures 1
NAS 1.26:183203 Airborne radar technology for windshear detection 1
NAS 1.26:183204 The high temperature creep deformation of Si₃N₄-6Y₂O₃-ZAI₂O₃ 1
NAS 1.26:183205 Dynamics and control of the orbiting grid structures and the synchronously deployable beam final report / 1
NAS 1.26:183206 Performance analysis of FDDI 1
NAS 1.26:183207 Telescience testbed pilot program interim report 1
NAS 1.26:183208 Superheavyweight missions SI vs DI ascent flight design options and recommendations 1