Spacecraft design
Resource Information
The concept Spacecraft design represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Spacecraft design
Resource Information
The concept Spacecraft design represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Spacecraft design
- Source
- nasat
95 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
- Apollo lightcraft project : prepared for the NASA/USRA Advanced Design Program, 3rd annual summer conference, Washington, D.C., June 17-19, 1987
- 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
- Computational structures technology for airframes and propulsion systems : proceedings of two workshops sponsored by the National Aeronautics and Space Administration, Washington, D.C., and the Center for Computational Structures Technology, University of Virginia, Hampton, Virginia, and held at Lewis Research Center, Cleveland, Ohio, June 26-27, 1991, and at Langley Research Center, Hampton, Virginia, September 4-5, 1991
- 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
- Development of integrated programs for aerospace-vehicle design (IPAD
- Dynamics and control of orbiting space structures, NASA advanced design program (ADP) : final report, grant NAGW-4252
- 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 for research study entitled "Performance evaluation of the Gravity Probe B design" : contract number--NAS8-40618
- Final report, NASA/USRA University Advanced Design Program at the University of Illinois for the 1989-1990 academic year
- Final report, impact of lunar and planetary missions on the space station
- 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
- Kinetic isolation tether experiment : annual report
- Mars Sample Return : Mars ascent vehicle mission & technology requirements
- Meteoroids and orbital debris : effects on spacecraft
- Microspacecraft and earth observation : electrical field (ELF) measurement project
- NASA in-house commercially developed space facility (CDSF) study report : concept configuration definition
- 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
- Power, propulsion, and communications for microspacecraft missions
- Preliminary structural sensitivity study of hypersonic inflatable aerodynamic decelerator using probabilistic methods
- Proceedings of the eighth annual Thermal and Fluids Analysis, Workshop, spacecraft analysis and design
- Propulsion options for primary thrust and attitude control of microspacecraft : prepared under contract NAS3-27186
- 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
- Spacecraft system integration and test : SSTI Lewis critical design audit
- Statistical analysis of a large sample size pyroshock test data set
- Statistical analysis of a large sample size pyroshock test data set including post flight data assessment
- Structural assembly demonstration experiment : final report for contract number NAS8-34501, Phase I
- Study of new systems concepts for a Titan atmospheric probe
- Surface nuclear power for human Mars missions
- System design under uncertainty : evolutionary optimization of the Gravity Probe-B spacecraft
- The Center for the Study of Terrestrial and Extraterrestrial Atmospheres (CSTEA) : NAGW 2950; five-year report, April 1992-December 1996
- The Magnetosphere Imager mission concept definition study final report
- 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
- The determination of operational and support requirements and costs during the conceptual design of space systems : final report : under grant no. NAG-1-1327
- The natural space environment : effects on spacecraft
- 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.umsl.edu/resource/UJOJFTyox1o/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.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.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
