Works matching DE "REUSABLE space vehicles"
Results: 37
Entire Flight Trajectory Design for Temporary Reconnaissance Mission.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 3, p. 137, doi. 10.2322/tjsass.60.137
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Shuttle at cruise speed.
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- Nature, 2008, v. 452, n. 7189, p. 794, doi. 10.1038/452794a
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THE TWO SHUTTLE ACCIDENT REPORTS: CONTEXT AND CULTURE IN TECHNICAL COMMUNICATION.
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- Journal of Technical Writing & Communication, 2006, v. 36, n. 3, p. 231, doi. 10.2190/0A9H-WN06-BQE2-W1EX
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SCIENCE IN SPACE VS SPACE SCIENCE: THE EUROPEAN UTILISATION OF SPACELAB.
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- History & Technology, 1999, v. 16, n. 2, p. 137, doi. 10.1080/07341519908581962
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- Article
Adaptive disturbance observer-based finite-time continuous fault-tolerant control for reentry RLV.
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- International Journal of Robust & Nonlinear Control, 2017, v. 27, n. 18, p. 4275, doi. 10.1002/rnc.3796
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retrospect.
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- Weatherwise, 2004, v. 57, n. 3, p. 18, doi. 10.1080/00431670409605454
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Comet Hale-Bopp (C/1995 O1): UVSTAR-FUV Spectroscopy from the Space Shuttle.
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- Astrophysics & Space Science, 2006, v. 301, n. 1-4, p. 135, doi. 10.1007/s10509-006-0180-z
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Attitude control of reusable launch vehicle in reentry phase with input constraint via robust adaptive backstepping control.
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- International Journal of Adaptive Control & Signal Processing, 2015, v. 29, n. 10, p. 1308, doi. 10.1002/acs.2541
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Thermo-structural Analysis of 3D Composites for Reusable Vehicle Applications.
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- International Journal of Vehicle Structures & Systems (IJVSS), 2011, v. 3, n. 4, p. 225, doi. 10.4273/ijvss.3.4.03
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Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV).
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- Advanced Composite Materials, 2001, v. 10, n. 4, p. 339, doi. 10.1163/156855101753415364
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Investigation of wing structure layout of aerospace plane based on the finite element method.
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- Advances in Mechanical Engineering (Sage Publications Inc.), 2017, v. 9, n. 7, p. 1, doi. 10.1177/1687814017713701
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NASA aims high for reusable spacecraft.
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- Nature, 1996, v. 382, n. 6587, p. 104, doi. 10.1038/382104a0
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THE SPACE SHUTTLE NASA's White Elephant in the Sky.
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- Bulletin of the Atomic Scientists, 1973, v. 29, n. 2, p. 36, doi. 10.1080/00963402.1973.11455448
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The Post-Apollo Era--Decisions Facing Nasa.
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- Bulletin of the Atomic Scientists, 1967, v. 23, n. 4, p. 11, doi. 10.1080/00963402.1967.11455052
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Shuttle Risk Progression -- Focus on Historical Risk Increases.
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- International Journal of Performability Engineering, 2013, v. 9, n. 6, p. 633
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Committing to the Shuttle Without Ever Having a National Policy.
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- Air Power History, 2005, v. 52, n. 3, p. 36
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WITNESS TO TRAGEDY: THE SHUTTLE COLUMBIA DISASTER.
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- East Texas Historical Journal, 2004, v. 42, n. 2, p. 3
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Sixteen Minutes to Eternity.
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- Quality Engineering, 2004, v. 16, n. 1, p. 9, doi. 10.1081/QEN-120020765
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Optimal Starting Conditions for the Rendezvous Maneuver, Part 2: Mathematical Programming Approach.
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- Journal of Optimization Theory & Applications, 2008, v. 137, n. 3, p. 625, doi. 10.1007/s10957-008-9356-8
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Optimal Starting Conditions for the Rendezvous Maneuver, Part 1: Optimal Control Approach.
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- Journal of Optimization Theory & Applications, 2008, v. 137, n. 3, p. 593, doi. 10.1007/s10957-007-9347-1
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Integrated guidance and control for reusable launch vehicle in reentry phase.
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- Nonlinear Dynamics, 2015, v. 80, n. 1/2, p. 397, doi. 10.1007/s11071-014-1877-0
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A Reliable Airline.
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- Harvard International Review, 1984, v. 6, n. 6, p. 37
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Risk Analysis of the Space Shuttle: Pre-Challenger Prediction of Failure.
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- 1989
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- Industry Overview
THERMAL PROTECTION TILE STRUCTURES OF SHUTTLECRAFT WITH DIFFERENT EXTERNAL LOAD-CARRYING ELEMENTS.
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- Paton Welding Journal, 2015, n. 3/4, p. 63, doi. 10.15407/tpwj2015.04.09
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Beyond the Widget.
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- Air & Space Power Journal, 2004, v. 18, n. 2, p. 31
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Observations of Typhoon Melissa during the Lidar In-Space Technology Experiment (LITE).
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- Journal of Applied Meteorology (1988), 2003, v. 42, n. 7, p. 1003, doi. 10.1175/1520-0450(2003)042<1003:OOTMDT>2.0.CO;2
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Space Shuttle Diplomacy.
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- Harvard International Review, 1980, v. 2, n. 6, p. 16
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Development and Ground Combustion Test of a Subscale Reusable Winged Rocket.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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Development of Main Propulsion System for Reusable Sounding Rocket: Design Considerations and Technology Demonstration.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
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The Space Shuttle Program and Its Support for Space Bioresearch.
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- BioScience, 1973, v. 23, n. 5, p. 307, doi. 10.2307/1296441
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Northrop Grumman-Boeing team shows Space Shuttle successor.
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- Advanced Materials & Processes, 2005, v. 163, n. 12, p. 52
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NASA approves new design for shuttle external tank fitting.
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- Advanced Materials & Processes, 2004, v. 162, n. 9, p. 31
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MATERIALS for Air and Space.
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- Advanced Materials & Processes, 2000, v. 158, n. 3, p. 63
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DEPENDABILITY ANALYSIS OF HYBRID REDUNDANCY SYSTEMS USING FUZZY APPROACH.
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- International Journal of Reliability, Quality & Safety Engineering, 2010, v. 17, n. 4, p. 331, doi. 10.1142/S0218539310003846
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Integrated electrohydraulic control actuation system with centralized power plant for the Reusable Launch Vehicle Technology Demonstrator.
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- Current Science (00113891), 2018, v. 114, n. 1, p. 84, doi. 10.18520/cs/v114/i01/84-100
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Development of slow-burning solid rocket booster for RLV-TD hypersonic experiment.
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- Current Science (00113891), 2018, v. 114, n. 1, p. 74, doi. 10.18520/cs/v114/i01/74-83
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An overview of Reusable Launch Vehicle Technology Demonstrator.
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- Current Science (00113891), 2018, v. 114, n. 1, p. 38, doi. 10.18520/cs/v114/i01/38-47
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- Article