The orbiting astronomical observatory /OAO/ STRUCTURE.
OAO structure for measuring absolute stellar energy in UV region
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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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OAO structure for measuring absolute stellar energy in UV region
Stability analysis algorithm for estimating equilibrium state of OAO control system
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Predicting structural response of OAO A-2 to transient loading at Atlas booster engine cut-off
Dimensional stability of construction materials for OAO
Algorithm development for estimating domain of attraction of OAO paired-tracker equilibrium state with Liapunov functions
Research activities of Lunar and Planetary Laboratory
Atlas Centaur 16 flight performance in injecting OAO-2 into nearly circular earth orbit
Thermal test and evaluation program for OAO 2
Stabilization and control system and mission operations for OAO
General purpose computer for onboard processing of data for OAO missions
Simulated jettisoning performance of Atlas Centaur nose fairing carrying OAO spacecraft
OAO thermal subsystem design to provide temperature control for experiments and spacecraft electronic devices
Multispectral UV sky mapping and heavenly body intensity measurement onboard OAO 2 satellite
UV photometry from OAO-2, describing Wisconsin instrumentation and equipment
Optimal quadratic Liapunov function generating algorithm for estimating domain of equilibrium attraction of nonlinear star tracker attitude control systems for OAO stability
Ni-Cd batteries for OAO 2 spacecraft, considering manufacturing, materials, components and tests
OAO 2 design and performance features concerning pointing accuracy and stability, command capability, data handling, thermal environment, orbit constraints, ultraviolet spectroscopy, etc