A Comparison of Damaging Meteoroid and Orbital Debris Fluxes in Earth Orbit
No abstract available
Cooke, William↗
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A Comparison of Damaging Meteoroid and Orbital Debris Fluxes in Earth Orbit
No abstract available
Cooke, William↗
SpaceOptical Communications using Laser Arrays for CubeSats in Low Earth Orbit (LEO) or Low Lunar Orbit (LLO)
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HECC↗
The Mars Reconnaissance Orbiter Mission: 10 years of exploration from Mars orbit
UNKNOWN
Zurek, Richard↗
Low-energy trajectories from geosynchronous transfer orbits to lunar libration orbits
No abstract provided
Wilson, Roby S↗
Aerocapture Trajectories for Earth Orbit Technology Demonstration and Orbiter Science Missions at Venus, Mars and Neptune
No abstract provided
Jadusingh, Matt↗
On-Orbit Cross Calibration Between the Osiris-Rex Orbiting Laser Altimeter and Navigation Camera
Accurate shape models of small bodies provide both science value and resources for precision relative navigation. One instrument commonly used for generating shape models is the laser altimeter. Laser altimeters require accurate intrinsic and extrinsic calibration knowledge to produce accurate shape models. Here, we describe a method used for updating the intrinsic and extrinsic calibration parameters of the laser altimeter onboard the Origins, Spectral Interpretation, Resource Identification, and Security–Regolith Explorer (OSIRIS-REx) spacecraft, OLA (OSIRISREx Laser Altimeter). We perform the calibration update by comparing the OLA scans with monocular camera images of the asteroid surface captured by the primary navigation camera.
Andrew J. Liounis↗
Orbital Debris, Space Situational Awareness, and Space Traffic Management - Managing Risks from Orbital Debris
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J.-C. Liou↗
Orbital Debris and the NASA Orbital Debris Program Office
This submission includes 11 presentations prepared by NASA for the Trilateral Safety & Mission Assurance (SMA) Conference from June 24-26th at the ESA Centre for Earth Observation. These presentations encompass various safety & mission assurance topics focused on the conference themes of lunar exploration, space sustainability, new commercial partners & challenges, digital engineering, and the assurance of new technologies. These presentations will be shared amongst an international community of SMA practitioners & leadership to promote mutual dialogue on initiatives & challenges of SMA in an evolving spaceflight field.
OSIRIS↗
Orbital Decay in an Accreting and Eclipsing 13.7 Minute Orbital Period Binary with a Luminous Donor
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Kevin B. Burdge↗