Launch vehicles (Astronautics)
Label
Launch vehicles (Astronautics)
Name
Launch vehicles (Astronautics)
Actions
Incoming Resources
- Subject of36
- Commercial Space Launch Act, report (to accompany H.R. 3942) (including cost estimate of the Congressional Budget Office)
- Possible deficiencies in predicting transonic aerodynamics on the X-43A, Steven G. Labbe, Michael G. Gilbert, Michael W. Kehoe
- A vision of future space transportation, a visual guide to future spacecraft concepts, by Tim McElyea; contributing editor, Robert Godwin
- Test report for MSFC test #83-2, pressure scaled water impact test of a 12.5 inch diameter model of the space shuttle solid rocket booster filament wound case and external TVC POD
- The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles, A.T. Nettles, A.J. Hodge, and J.R. Jackson
- Applying Monte Carlo simulation to launch vehicle design and requirements analysis, J.M. Hansen and B.B. Beard
- Proceedings of the Workshop on Identification and Control of Flexible Space Structures, G. Rodriguez, editor
- SEE design guide and requirements for electrical deadfacing, J.M. Berki, N.B. Sargent
- Space shuttle phase B wind tunnel model and test information, J.L. Glynn and D.E. Poucher, Volume 3
- Guide to probability of failure analysis for new expendable launch vehicles
- Commercial space launches, report (to accompany H.R. 3942)
- The mighty Saturns, a presentation of Spacecraft Films ; written and produced by Mark Gray, Part 1
- ACT payload shroud structural concept analysis and optimization, Bart F. Zalewski, Brett A. Bednarcyk ; prepared for the 16th U.S. National Congress on Theoretical and Applied Mechanics (USNCTAM) sponsored by the U.S. Committee on Theoretical and Applied Mechanics, University Park, Pennsylvania, June 27-July 2, 2010
- Liquid oxygen propellant densification production and performance test results with a large-scale flight-weight propellant tank for the X33 RLV, Thomas M. Tomsik and Michael L. Meyer
- Space shuttle phase B wind tunnel model and test information, J.L. Glynn and D.E. Poucher, Volume 1
- Rationales for the Lightning Flight-Commit Criteria, John C. Willett [and others]
- SRM-assisted trajectory for the GTX reference vehicle, John Riehl and Charles Trefny, Daniel Kosareo
- Two-stage reusable launch system utilizing a winged core vehicle and glideback boosters, Ian O. MacConochie [and others]
- Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications, A.T. Nettles
- Staffing of the expendable launch vehicle program office at the Kennedy Space Center
- Three dimensional numerical simulation of rocket-based combined-cycle engine response during mode transition events, Jack R. Edwards, D. Scott McRae, and Ryan B. Bond
- Ares I-X flight test vehicle, stack 5 modal test, Ralph D. Buehrle [and others]
- Initial assessment of the Ares I-X launch vehicle upper stage to vibroacoustic flight environments, Jeffrey M. Larko and William O. Hughes ; prepared for the14th International Congress on Sound Vibration (ICSV14) cosponsored by the International Institute of Acoustics and Vibration (IIAV) and the Australian Acoustical Society (AAS), Cairns, Australia, July 9-12, 2007
- Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods, Gary E. Erickson
- Report of Apollo 13 Review Board, [Edgar M. Cortright, chairman]
- Closed-loop simulation study of the Ares I upper stage thrust vector control subsystem for nominal and failure scenarios, Amy Chicatelli [and others]
- Concepts of operations for a reusable launch vehicle, Michael A. Rampino
- Design of 8-ft-diameter barrel test article attachment rings for Shell Buckling Knockdown Factor Project, Andrew E. Lovejoy and Mark W. Hilburger
- Peer review of launch environments, Timmy R. Wilson
- Commercial Space Launch Act amendments of 1988, report (to accompany H.R. 4399) (including cost estimate of the Congressional Budget Office)
- A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept, B. Spencer, Jr., C.H. Fox, Jr., and J.K. Huffman
- Approximate pressure distribution in an accelerating launch-vehicle fuel tank, Michael P. Nemeth
- Ares I-X flight test vehicle, stack 1 modal test, Ralph D. Buehrle [and others]
- Delta II launch vehicle
- Saturn V Flight Manual, Astronaut's Guide to the Apollo Moon Rocket, Progressive Management
- COMPASS final report, low cost Robotic Lunar Lander, Melissa L. McGuire and Steven R. Oleson