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PRESS CONFERENCE- TIROS I
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Conference on space, science, and urban life, dunsmuir house, oakland, california, march 28-30, 1963 proceedings
Use of space age science and technology to solve socioeconomic problems of metropolitan areas resulting from industrial.
Proceedings of the conference on the law of space and of satellite communications
Space law and communications satellites, free space lower boundary, control of space, orbital regulation, and international cooperation.
Ranger vii preliminary results conference, jet propulsion laboratory, pasadena, california
Discussion of preliminary results of ranger vii lunar probe
Address by james e. webb, administrator, national aeronautics and space administration midwest governors' conference, minneapolis, minnesota, september 10, 1964 news release
Solving economic problems of midwest through joint efforts of industries and universities as related to nasa programs
Testing of manned flight systems conference.
Papers concerning flight testing and simulation programs for evaluating manned aerospace systems
Nasa press conference on findings of explorer vi, 28 september 1959
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Press conference, 7 august 1959. explorer vi
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Proceedings of First National Conference on the Peaceful Uses of Space
No abstract available
Explorer x press conference, 18 april 1961 news release no. 61-83
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Lunar sciences press conference
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Ranger viii post-impact press conference news release
Ranger VIII photographs of lunar surface
Mariner iv interim science findings, news conference news release
Mariner IV space probe - instrumentation, trajectory, and experiments
Brief for conference on oceanographic exploration from satellites
Sea surface observations from satellites for oceanographic explorations - applications to radiometry, currents, topography, sea level and gravity, and geomagnetism
Proceedings of the apollo unified s-band technical conference
Tracking and communications system for Apollo spacecraft at lunar distances using S-band
NACA Conference on Aerodynamic Problems of Transonic Airplane Design
During the past several years it has been necessary for aeronautical research workers to exert a good portion of their effort in developing the means for conducting research in the high-speed range. The transonic range particularly has presented a very acute problem because of the choking phenomena in wind tunnels at speeds close to the speed of sound. At the same time, the multiplicity of design problems for aircraft introduced by the peculiar flow problems of the transonic speed range has given rise to an enormous demand for detail design data. Substantial progress has been made, however, in developing the required research techniques and in supplying the demand for aerodynamic data required for design purposes. In meeting this demand, it has been necessary to resort to new techniques possessing such novel features that the results obtained have had to be viewed with caution. Furthermore, the kinds of measurements possible with these various techniques are so varied that the correlation of results obtained by different techniques generally becomes an indirect process that can only be accomplished in conjunction with the application of estimates of the extent to which the results of measurements by any given technique are modified by differences that are inherent in the techniques. Thus, in the establishment of the validity and applicability of data obtained by any given technique, direct comparisons between data from different sources are a supplement to but not a substitute for the detailed knowledge required of the characteristics of each technique and fundamental aerodynamic flow phenomena.