The X-Ray Surveyor: Mission Concept, Strawman Mission Design, and Preliminary Cost Estimate
No abstract available
The X-ray Surveyor↗
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Results for “Mission design”
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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Mission Design Analysis for the Martian Moon Phobos: Close Flybys, Missed Thrusts, and Other In-Flight Entertainment
No abstract available
Stuart, Jeffrey↗
DARE Mission Design: Low RFI Observations from a Low-Altitude Frozen Lunar Orbit
The Dark Ages Radio Explorer (DARE) seeks to study the cosmic Dark Ages approximately 80 to 420 million years after the Big Bang. Observations require truly quiet radio conditions, shielded from Sun and Earth electromagnetic (EM) emissions, on the far side of the Moon. DAREs science orbit is a frozen orbit with respect to lunar gravitational perturbations. The altitude and orientation of the orbit remain nearly fixed indefinitely, maximizing science time without the need for maintenance. DAREs observation targets avoid the galactic center and enable investigation of the universes first stars and galaxies.
Plice, Laura↗
MONTE: The Next Generation of Mission Design and Navigation Software
No abstract available
Evans, Scott E.↗
HelioSwarm: Mission Design Considerations for a SmallSat Swarm in High Earth Orbit
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Stephen West↗
Human Landing System Storable Propellant Architectures: Mission Design, Guidance, Navigation, and Control
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Scott Craig↗
A New Concurrent Engineering Tool for the Mission Design Center at NASA Ames
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David Mauro↗
Application of a large space-based diffractive optical element telescope to the Terrestrial Planet-Finder Mission: design and tolerance issues
An analytical description of the scattered light from a 10 meter diameter Diffractive Optical Element lens-based telescope operating at 1 micron wavelength has been formulated.
DOE↗
Genesis Mission Design
The Genesis spacecraft will collect solar wind samples from a halo orbit about the Sun-Earth L1 point for two years, returning those samples to Earth in 2003 for on-Earth analysis and examination.
Genesis↗
The LISA Mission Design
The Laser Interferometer Space Antenna (LISA) will be capable of detecting gravitational waves with frequencies from 0.1 mHz to 1 Hz by using laser interferometers to monitor changes in the distances between test masses in spacecraft separated by five million km.
Laser↗