Ranger tv subsystem.
Six-camera two channel television subsystem designed for use in Ranger VI through IX SPACECRAFT
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Six-camera two channel television subsystem designed for use in Ranger VI through IX SPACECRAFT
Solar cosmic rays associated with meter Type VI RADIO burst confirmed from data from 21 stations
Rangers VI through IX TV subsystem testing under simulation of Atlas and Agena launch characteristics, midcourse motor action and deep space environment
Since September of 1956, nine Jupiter-C missiles have been launched from the firing pad at Cape Canaveral. The first Jupiter-C firing tested the propulsion system, air frame, and guidance components of the missile, and the second and third firings tested a model of the Jupiter nose cone under realistic re-entry conditions. The remaining six Jupiter-C missiles were used as the launching vehicles for EXPLORER satellites I through VI (Fig. 1). Of the six satellite firings, EXPLORERs I, III, and IV achieved satisfactory orbits. The Jupiter-C missile was designed and developed as a joint program under the technical direction of the Jet Propulsion Laboratory and the Army Ballistic Missile Agency. The Jet Propulsion Laboratory developed the three high-speed stages, and the Army Ballistic Missile Agency handled the development, construction, and operation of the first-stage booster rocket and the guidance system. Many other organizations have contributed to the success of the EXPLORER satellite program, most notably the State University of Iowa, the Air Force Cambridge Research Center, and the satellite tracking teams of the Vanguard organization.
Synoptic terrain color photography on Gemini VI- AND VII missions
Interplanetary magnetic field measurements using flux gate magnetometer sensor mounted on Pioneer VI space probe, noting various graphs
Collimation of cosmic rays by interplanetary magnetic field based on Pioneer VI measurements during flare event
Compositional, anisotropic and nonradial flow characteristics of solar wind as observed by ARC HIGH-RESOLUTION Pioneer VI plasma probe
Gemini VII star sightings analyzed, using handheld space sextant in Gemini VI, discussing effect of bias, timing, angle measurement and trajectory errors
Shutters, lenses, vidicons, data rates and calibration techniques for TV cameras of Rangers VI, VII, VIII and IX
Deep Space Stations flight support operations for Surveyor II, Lunar Orbiter I, Pioneer VI and VII, Mariner IV, and Atlas Centaur
Molecular orbital techniques used to find cubic field splitting 3a of certain ions in periodic group II-VI compounds of T sub d symmetry
Nonmagnetic, explosive-actuated indexing device for magnetometer experiment aboard Pioneer VI AND VII spacecrafts
Missions of Gemini VI through XI covering rendezvous, docking, thermal overloading, translation maneuver, etc
Anisotropic proton velocity distribution obtained from solar wind measurements on Pioneer VI SPACECRAFT
Aspect system on Pioneer VI and VII INCORPORATES digital computer for accurate time sector division of spin stabilized vehicle
Gemini VII star sightings analyzed, using handheld space sextant in Gemini VI, discussing effect of bias, timing angle measurement and trajectory errors