Atlas-Centaur VI flight path and its determination from tracking data
Atlas Centaur spacecraft trajectory in earth orbit and tracking data reduction method
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Atlas Centaur spacecraft trajectory in earth orbit and tracking data reduction method
Postflight trajectory reassembly analysis of Atlas Centaur flight AC-6
Preflight and flight activities of Gemini 10 launch - tracking, crew training, mission profile, and times of major events
Selection of elliptic orbit for solar probe craft without undue perihelion growth
Coast-phase propellant management system for two- burn Atlas-Centaur flight AC-8
Atlas-Centaur-Surveyor range safety data - trajectory characteristics, impact locations for jettisoned items, and destruct data
Atlas Centaur flight wind launch restriction backup procedure
Atlas Centaur pad safety report for launch complex 36A and 36B
Mariner Venus project design changes for flyby mission and sensing of Venus atmosphere
Mariner Mars 1969 project and spacecraft design modifications for flyby missions
Simulated coasting flight test on sensing tip of liquid-vapor sensor for liquid hydrogen fuel tank
Mission, launch and test operations, and communications for Atlas Agena-18 with lunar Orbiter B
Launch and flight data, data acquisition, and prelaunch operations summaries for Lunar Orbiter A launching with Atlas Agena 17
Network performance analysis for Gemini GTA-8 MISSION
Dynamics tests of engine-structure coupled longitudinal oscillations of Atlas Centaur Surveyor
Comet missions, discussing spacecraft exploration criteria for short period and long period first- apparition comets
To be placed into a highly elliptical transfer orbit by the Atlas Centaur (AC-61) launch vehicle, the INTELSAT V-F satellite has 12,000 voice circuits and 2 color television channels and incorporates a maritime communication system for ship to shore communications. The stages of the launch vehicle and the launch operations are described. A table shows the launch sequence.
Various papers on the ELV payload environment are presented. Individual topics addressed include: EnviroNET: the Space Environment Information Service, ELV Payload Environments Study, perspective of GSFC Orbital Launch Services Office, Cosmic Background Explorer, the Standard Booster Interface, MLV Standard Interface Study, future payload requirements, General Dynamics Atlas family, Delta II Launch Vehicle environments, Titan vibroacoustics, Titan IV, the Scout Launch Vehicle, Pegasus.