Project fire integrated post flight evaluation report, flight no. 1
Fire project flight test of Atlas launch vehicle, Antares velocity package, and reentry vehicle
ANTARES MISSILE↗
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Results for “ATLAS”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Thermal conditions during typical boost trajectory
Aerodynamic heating calculation of Atlas Centaur launch vehicle trajectory
TRAJECTORY↗
Surveyor launch opportunities for mid-1965 through 1968
Lunar launch data - ascent characteristics of Atlas-Centaur AC-15 configuration and mission ground rules applied to models for Surveyor flights
LUNAR LAUNCH↗
Mariner mars 1969 orbiter technical feasi- bility study
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineering results reported
PLANETARY ORBIT↗
An analysis of chemical upper stages for nasa scientific missions
Analysis of chemical upper stage of launch vehicles - Hydrogen-oxygen upper stage for Atlas-Centaur and Saturn IB-Centaur launch vehicle - Hydrogen-fluorine propellants
HYDROGEN FLUORIDE↗
Centaur electrical system problems, related work, and solutions
Atlas Centaur electrical equipment problems - silver-zinc batteries and static inverter
ATLAS CENTAUR LAUNCH VEHICLE↗
Conceptual study of a micrometeoroid deep space satellite. volume iii- orbital mechan- ics, power supply and distribution, vehicle design, thermal control, attitude sensing and determination final report
Satellite design for deep space micrometeoroid study - selection of Atlas-Agena launch vehicle, power supply, and attitude control
MICROMETEOROID↗
Environmental test program - ranger tv system.
Rangers VI through IX TV subsystem testing under simulation of Atlas and Agena launch characteristics, midcourse motor action and deep space environment
ATLAS AGENA LAUNCH VEHICLE↗
Surveyor project status report, 13 November 1964
Soft landing on moon by spacecraft, Atlas Centaur launch vehicle - Surveyor project
SPACECRAFT↗
Explicit guidance equations for multistage boost trajectories
Explicit equations for steering Atlas-Centaur multistage launch vehicle to lunar trajectory
MULTISTAGE VEHICLE↗
Ranger VIII and IX. Part I - Mission description and performance
Ranger VIII and Ranger IX mission - pre-launch and launch operations, Atlas Agena launch vehicle system, deep space network, flight path, flight operations, and spacecraft subsystems
ATLAS AGENA LAUNCH VEHICLE↗
Effect of pitch program variations on launch availability of Atlas/Centaur-AC-7 to AC-15
Pitch programs for Atlas Centaur vehicle launch times based on wind profile data
LAUNCH DATE↗
Ground-wind restrictions procedure for Atlas/Centaur/Surveyor AC-6 and AC-7
Surface wind restrictions for Atlas Centaur launch vehicle while erected on launching pad
WIND↗
Postflight trajectory reassembly AC-6
Postflight trajectory reassembly analysis of Atlas Centaur flight AC-6
COMPUTER SIMULATION↗
Origin of high-intensity noise in the area of a large protuberance on a launch vehicle
Origin of high intensity noise in area of large protuberance on Atlas-Agena-Mariner C model tested in supersonic wind tunnel
SCALE MODEL↗
Lunar Orbiter Flight Set for August
Lunar orbiter A - configuration, tasks, Atlas Agena launch vehicle, data acquisition and evaluation, and mission events
SPACECRAFT CONFIGURATION↗
The neutron flux in space following a polar cap neutron event on November 15, 1960
A neutron detector flown on an Atlas pod during the 15 November 1960 solar event measured a larger neutron flux than another detector flown on a similar vehicle during a quiet solar period. The excess neutron flux at low latitudes obtained by comparing these two measurements is about an order of magnitude higher than expected from the neutron production in the atmosphere by solar protons as deduced from Lingenfelter's calculations and Webber's model for the 15 November event. It is suggested that most of the discrepancy can be accounted for by considering neutron production by energetic solar alpha particles and lowered geomagnetic cutoffs.
NEUTRON FLUX↗
U.S. to Launch Most Advanced Unmanned Spacecraft
Characteristics of OAO-A1 unmanned spacecraft and Atlas-Agena launch vehicle
UNMANNED SPACECRAFT↗