Spacecraft design
Resource Information
The concept Spacecraft design represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
The Resource
Spacecraft design
Resource Information
The concept Spacecraft design represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
- Label
- Spacecraft design
- Source
- nasat
80 Items that share the Concept Spacecraft design
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- Working on the boundaries : philosophies and practices of the design process
- "The Gevaltig" : an inertial fusion powered manned spacecraft design for outer solar system missions
- 3D space radiation transport in a shielded ICRU tissue sphere
- A 3DHZETRN code in a spherical uniform sphere with Monte Carlo verification
- A computer-based orbital debris environment model for spacecraft design and observation in low earth orbit
- A method of isolating treadmill shock and vibration on spacecraft
- A method of isolating treadmill shock and vibration on spacecraft
- Additive manufacturing, an enabling technology for the MoonBeam 6U CubeSat mission
- Advanced orbit transfer vehicle propulsion system study : final report
- Advanced x-ray timing array mission : conceptual spacecraft design study
- Aerobrake assembly with minimum space station accommodation
- Aerospace vehicle design : spacecraft section : final project reports
- Aerothermal analysis and design of the Gravity Recovery and Climate Experiment (GRACE) spacecraft
- Aerothermal analysis and design of the Gravity Recovery and Climate Experiment (GRACE) spacecraft
- Alternate space station Freedom configuration considerations to accommodate solar dynamic power
- An optimization-based integrated controls-structures design methodology for flexible space structures
- Artemis sustained translational acceleration limits : human tolerance evidence from Apollo to International Space Station
- Autonomous space processor for orbital debris : final report (1989-90)
- Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel
- Comparison of separation shock for explosive and nonexplosive release actuators on a small spacecraft panel
- Conceptual launch vehicle and spacecraft design for risk assessment
- Concurrent mission and systems design at NASA Glenn Research Center : the origins of the COMPASS team
- Conventional and bimodal nuclear thermal rocket (NTR) artificial gravity Mars transfer vehicle concepts
- Cooper-Harper experience report for spacecraft handling qualities applications
- Crew emergency return vehicle autoland feasibility study
- Cryogenic on-orbit liquid depot-storage, acquisition and transfer (COLD-SAT) experiment conceptual design and feasibility study
- Design and fabrication of the NASA HL-20 full scale research model
- Design of an autonomous teleoperated cargo transporting vehicle for lunar base operations
- Design study for the asteroid redirect vehicle (ARV) composite primary bulkhead
- Design study of an integrated aerobraking orbital transfer vehicle
- Development of integrated programs for aerospace-vehicle design (IPAD
- Evaluation of the NASA arc jet capabilities to support mission requirements
- Evolutionary growth for space station Freedom electrical power system
- Examination of the structural response of the Orion European service module to reverberant and direct field acoustic testing
- Experimenter's data package for the descending layers rocket project initiation conference
- External tank gamma ray imaging telescope study : final review, phase II
- Feasibility of large high-powered solar electric propulsion vehicles : issues and solutions
- Final report, NASA/USRA University Advanced Design Program at the University of Illinois for the 1989-1990 academic year
- Final study report for the space shuttle Ii advanced space transportation system
- Galileo : earth avoidance study report
- Geopotential Research Mission, science, engineering, and program summary
- Geopotential Research Mission, science, engineering, and program summary
- Human factors in space station architecture I : space station program implications for human factors research
- Indium tin oxide-magnesium fluoride co-deposited films for spacecraft applications
- Indium tin oxide-magnesium fluoride co-deposited films for spacecraft applications
- Integrated controls-structures design methodology for flexible spacecraft
- MISSE-flight facility polymers and composites experiment 1-4 (PCE 1-4)
- Mars Sample Return : Mars ascent vehicle mission & technology requirements
- Microspacecraft and earth observation : electrical field (ELF) measurement project
- NASA in-house commercially developed space facility (CDSF) study report : concept configuration definition
- NASA lunar lander reference design
- NASA reliability preferred practices for design and test
- Orbital debris research at NASA Johnson Space Center, 1986-1988
- Packaging, deployment, and on-orbit assembly options for large geostationary spacecraft
- Preliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods
- Report of the Group Task Force on Satellite Rescue and Repair
- Report on final recommendations for IMPS engineering/science payload
- Report on orbital debris
- Report to the President : actions to implement the recommendations of the Presidential Commission on the Space Shuttle Challenger Accident
- Requirements for multidisciplinary design of aerospace vehicles on high performance computers
- Reusable Reentry Satellite (RRS) summary report : launch tradeoff study
- Robust control of nonlinear flexible multibody systems using quaternion feedback and dissipative compensation
- Space Shuttle Technical Conference : papers
- Space Transfer Vehicle Concepts and Requirements Study, Volume II | Book 2, Appendix
- Space station cathode design, performance, and operating specifications
- Space station definition, design, and development : manipulator design methodology, Task 5: Multiple arm telerobot coordination and control
- Spacecraft expected cost analysis with k-out-of-n:G subsystems
- Statistical analysis of a large sample size pyroshock test data set including post flight data assessment
- Study of new systems concepts for a Titan atmospheric probe
- Surface nuclear power for human Mars missions
- The NASA controls-structures interaction technology program
- The PI-mode of project management
- The aerobraking space transfer vehicle
- The conductor-dielectric junctions in a low density plasma
- The conductor-dielectric junctions in a low density plasma
- Thermal analysis research applicable to space station technology needs
- Vehicle and mission design options for the human exploration of Mars/Phobos using "Bimodal" NTR and LANTR propulsion
- Vehicle and mission design options for the human exploration of Mars/Phobos using "Bimodal" NTR and LANTR propulsion
- Vibration characteristics of a steadily rotating slender ring
- Wide field x-ray telescope mission concept study results
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/UJOJFTyox1o/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/UJOJFTyox1o/">Spacecraft design</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
