Flight-wind restrictions procedure, Atlas/ Centaur AC-6 through AC-15
Prelaunch calculation of wind profile effect using axial load and bending moments for Atlas and Centaur launch vehicles
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Prelaunch calculation of wind profile effect using axial load and bending moments for Atlas and Centaur launch vehicles
Fluorine-liquid oxygen disconnect for Atlas launch vehicle oxidizer system
Protecting fluorine-liquid oxygen Atlas launch vehicle oxidizer tank against overpressurization
Evaluation of Mars 7G1 auxiliary rocket motor for use as retrograde thrust generator on Atlas-Centaur space vehicle
Atlas Centaur spacecraft trajectory in earth orbit and tracking data reduction method
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
Postflight analysis of AC-8 Atlas Centaur vehicle with Surveyor payload model
Stage separation dynamics and system related to staging of Atlas Centaur launch vehicle - full scale model tests
Mission, launch and test operations, and communications for Atlas Agena-18 with lunar Orbiter B
Dynamics tests of engine-structure coupled longitudinal oscillations of Atlas Centaur Surveyor
Applications Technology Satellite-1 Atlas Agena launch vehicle flight performance evaluation
Shroud for Lunar Orbiter atop Atlas-Agena launch vehicle, noting structural alloys used
Optimization of Atlas-Agena trajectories via steepest ascent computer program
The newly developed 1/4 degrees World Ocean Atlas (WOA, Boyer and Levitus, 1998) is compared with the 1 degree WOA (Levitus et al., 1994) over the North Atlantic Ocean.
The Molecular Adsorber Coating (MAC) is a sprayable coatings technology that was developed at NASA Goddard Space Flight Center (GSFC). The coating was designed to address molecular contamination concerns on or near sensitive surfaces and instruments within the spacecraft for flight or ground-based applications in vacuum conditions. This paper will discuss the use of NASA's MAC technology to isolate and protect the critical laser flight optics of the Advanced Topographic Laser Altimeter System (ATLAS) instrument on the Ice, Cloud, and land Elevation Satellite-2 (ICESat-2). MAC was strategically used during thermal vacuum (TVAC) testing efforts to reduce the risk of contaminating the laser optical components from non-baked items and other unknown outgassing sources from the chamber environment. This paper summarizes the design and implementation efforts, and the chemical analysis of the MAC samples that were used during two recent TVAC tests for the ICESat-2/ATLAS mission.
The Molecular Adsorber Coating (MAC) is a sprayable coatings technology that was developed at NASA Goddard Space Flight Center (GSFC). The coating was designed to address molecular contamination concerns on or near sensitive surfaces and instruments within the spacecraft for flight or ground-based applications in vacuum conditions. This paper will discuss the use of NASA's MAC technology to isolate and protect the critical laser flight optics of the Advanced Topographic Laser Altimeter System (ATLAS) instrument on the Ice, Cloud, and land Elevation Satellite-2 (ICESat-2). MAC was strategically used during thermal vacuum (TVAC) testing efforts to reduce the risk of contaminating the laser optical components from non-baked items and other unknown outgassing sources from the chamber environment. This paper summarizes the design and implementation efforts, and the chemical analysis of the MAC samples that were used during two recent TVAC tests for the ICESat-2/ATLAS mission.
Poster: "What is ATLAS" "Calibration Summary" "Pre-Launch Calibration" "What is ICESat-2" "Acknowledgments" "Resources"