Works matching DE "REUSABLE space vehicles"

Results: 38

THERMAL PROTECTION TILE STRUCTURES OF SHUTTLECRAFT WITH DIFFERENT EXTERNAL LOAD-CARRYING ELEMENTS.

Published in:

Paton Welding Journal, 2015, n. 3/4, p. 63, doi. 10.15407/tpwj2015.04.09

By:

TIKHY, V. G.;
GUSEV, V. V.;
POTAPOV, A. M.;
SHEVTSOV, E. I.;
GUSAROVA, I. A.;
MANKO, T. A.;
FALCHENKO, Yu. V.

Publication type:

Article

SCIENCE IN SPACE VS SPACE SCIENCE: THE EUROPEAN UTILISATION OF SPACELAB.

Published in:

History & Technology, 1999, v. 16, n. 2, p. 137, doi. 10.1080/07341519908581962

By:

Russo, Arturo

Publication type:

Article

Beyond the Widget.

Published in:

Air & Space Power Journal, 2004, v. 18, n. 2, p. 31

By:

Deal, Duane W.

Publication type:

Article

Shuttle Risk Progression -- Focus on Historical Risk Increases.

Published in:

International Journal of Performability Engineering, 2013, v. 9, n. 6, p. 633

By:

HAMLIN, T. L.

Publication type:

Article

Observations of Typhoon Melissa during the Lidar In-Space Technology Experiment (LITE).

Published in:

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

By:

Kovacs, Thomas A.;
McCormick, M. Patrick

Publication type:

Article

The Space Shuttle Program and Its Support for Space Bioresearch.

Published in:

BioScience, 1973, v. 23, n. 5, p. 307, doi. 10.2307/1296441

By:

Mason, J. A.;
Heberlig, J. C.

Publication type:

Article

An overview of Reusable Launch Vehicle Technology Demonstrator.

Published in:

Current Science (00113891), 2018, v. 114, n. 1, p. 38, doi. 10.18520/cs/v114/i01/38-47

By:

Sivan, K.;
Pandian, S.

Publication type:

Article

Integrated electrohydraulic control actuation system with centralized power plant for the Reusable Launch Vehicle Technology Demonstrator.

Published in:

Current Science (00113891), 2018, v. 114, n. 1, p. 84, doi. 10.18520/cs/v114/i01/84-100

By:

Masilamani, V.;
Kumar, Manoj;
Narayan, S. Sankar;
Raghu, N.;
Namboodiripad, M. N.;
Mookiah, T.

Publication type:

Article

Development of slow-burning solid rocket booster for RLV-TD hypersonic experiment.

Published in:

Current Science (00113891), 2018, v. 114, n. 1, p. 74, doi. 10.18520/cs/v114/i01/74-83

By:

Parhi, Achutananda;
Mahesh, V.;
Kalluru, Khadarvoli;
Reshmi, S.;
Harikrishnan, R.;
Lakshmi, V. M.;
Murugan, J. Paul;
Reddy, Renjith Kumar

Publication type:

Article

WITNESS TO TRAGEDY: THE SHUTTLE COLUMBIA DISASTER.

Published in:

East Texas Historical Journal, 2004, v. 42, n. 2, p. 3

By:

Bradford, Dennis

Publication type:

Article

NASA aims high for reusable spacecraft.

Published in:

Nature, 1996, v. 382, n. 6587, p. 104, doi. 10.1038/382104a0

By:

Reichhardt, Tony

Publication type:

Article

Entire Flight Trajectory Design for Temporary Reconnaissance Mission.

Published in:

Transactions of the Japan Society of Aeronautical & Space Science, 2017, v. 60, n. 3, p. 137, doi. 10.2322/tjsass.60.137

By:

Mingpei LIN;
Ming XU

Publication type:

Article

Investigation of wing structure layout of aerospace plane based on the finite element method.

Published in:

Advances in Mechanical Engineering (Sage Publications Inc.), 2017, v. 9, n. 7, p. 1, doi. 10.1177/1687814017713701

By:

Yu Wang;
Lei Liu;
Yu Xing;
Zhenbo Yang

Publication type:

Article

Comet Hale-Bopp (C/1995 O1): UVSTAR-FUV Spectroscopy from the Space Shuttle.

Published in:

Astrophysics & Space Science, 2006, v. 301, n. 1-4, p. 135, doi. 10.1007/s10509-006-0180-z

By:

Cosmovici, Cristiano B.;
Bratina, Vojko;
Schwarz, Gottfried;
Tozzi, Gianpaolo;
Mumma, Michael J.;
Stalio, Roberto

Publication type:

Article

Adaptive disturbance observer-based finite-time continuous fault-tolerant control for reentry RLV.

Published in:

International Journal of Robust & Nonlinear Control, 2017, v. 27, n. 18, p. 4275, doi. 10.1002/rnc.3796

By:

Dong, Qi;
Zong, Qun;
Tian, Bailing;
Zhang, Chaofan;
Liu, Wenjing

Publication type:

Article

A Reliable Airline.

Published in:

Harvard International Review, 1984, v. 6, n. 6, p. 37

By:

Stark, Rick

Publication type:

Article

Space Shuttle Diplomacy.

Published in:

Harvard International Review, 1980, v. 2, n. 6, p. 16

By:

Brimmer, Philip

Publication type:

Article

DEPENDABILITY ANALYSIS OF HYBRID REDUNDANCY SYSTEMS USING FUZZY APPROACH.

Published in:

International Journal of Reliability, Quality & Safety Engineering, 2010, v. 17, n. 4, p. 331, doi. 10.1142/S0218539310003846

By:

CHELLAPPAN, C.;
VIJAYALAKSHMI, G.

Publication type:

Article

Optimal Starting Conditions for the Rendezvous Maneuver, Part 2: Mathematical Programming Approach.

Published in:

Journal of Optimization Theory & Applications, 2008, v. 137, n. 3, p. 625, doi. 10.1007/s10957-008-9356-8

By:

Miele, A.;
Ciarcià, M.

Publication type:

Article

Optimal Starting Conditions for the Rendezvous Maneuver, Part 1: Optimal Control Approach.

Published in:

Journal of Optimization Theory & Applications, 2008, v. 137, n. 3, p. 593, doi. 10.1007/s10957-007-9347-1

By:

Miele, A.;
Ciarcià, M.

Publication type:

Article

The Use of Perturbation with Monte Carlo Simulation Approach to Estimate the Reliability of the Space Shuttle Field Joints.

Published in:

International Journal for Computational Methods in Engineering Science & Mechanics, 2015, v. 16, n. 6, p. 313, doi. 10.1080/15502287.2015.1080320

By:

Jenab, Karoush;
Nicoll, Thomas

Publication type:

Article

Sixteen Minutes to Eternity.

Published in:

Quality Engineering, 2004, v. 16, n. 1, p. 9, doi. 10.1081/QEN-120020765

By:

Caplan, Frank

Publication type:

Article

THE SPACE SHUTTLE NASA's White Elephant in the Sky.

Published in:

Bulletin of the Atomic Scientists, 1973, v. 29, n. 2, p. 36, doi. 10.1080/00963402.1973.11455448

By:

O'Leary, Brian

Publication type:

Article

The Post-Apollo Era--Decisions Facing Nasa.

Published in:

Bulletin of the Atomic Scientists, 1967, v. 23, n. 4, p. 11, doi. 10.1080/00963402.1967.11455052

By:

Brown, Allan H.

Publication type:

Article

Risk Analysis of the Space Shuttle: Pre-Challenger Prediction of Failure.

Published in:

1989

By:

Dalal, Siddhartha R.;
Fowikes, Edward B.;
Hoadley, Bruce

Publication type:

Industry Overview

Shuttle at cruise speed.

Published in:

Nature, 2008, v. 452, n. 7189, p. 794, doi. 10.1038/452794a

By:

Schiermeier, Quirin

Publication type:

Article

THE TWO SHUTTLE ACCIDENT REPORTS: CONTEXT AND CULTURE IN TECHNICAL COMMUNICATION.

Published in:

Journal of Technical Writing & Communication, 2006, v. 36, n. 3, p. 231, doi. 10.2190/0A9H-WN06-BQE2-W1EX

By:

DOMBROWSKI, PAUL M.

Publication type:

Article

Attitude control of reusable launch vehicle in reentry phase with input constraint via robust adaptive backstepping control.

Published in:

International Journal of Adaptive Control & Signal Processing, 2015, v. 29, n. 10, p. 1308, doi. 10.1002/acs.2541

By:

Wang, Fang;
Hua, Changchun;
Zong, Qun

Publication type:

Article

Thermo-structural Analysis of 3D Composites for Reusable Vehicle Applications.

Published in:

International Journal of Vehicle Structures & Systems (IJVSS), 2011, v. 3, n. 4, p. 225, doi. 10.4273/ijvss.3.4.03

By:

Santhosh, B.;
Nandakumar, C. G.;
Sundararajan, S.

Publication type:

Article

Northrop Grumman-Boeing team shows Space Shuttle successor.

Published in:: Advanced Materials & Processes, 2005, v. 163, n. 12, p. 52
Publication type:: Article

Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV).

Published in:

Advanced Composite Materials, 2001, v. 10, n. 4, p. 339, doi. 10.1163/156855101753415364

By:

Morino, Y.;
Shimoda, T.;
Morimoto, T.;
Ishikawa, T.;
Aoki, T.

Publication type:

Article

retrospect.

Published in:

Weatherwise, 2004, v. 57, n. 3, p. 18, doi. 10.1080/00431670409605454

By:

Potter, Sean

Publication type:

Article

Integrated guidance and control for reusable launch vehicle in reentry phase.

Published in:

Nonlinear Dynamics, 2015, v. 80, n. 1/2, p. 397, doi. 10.1007/s11071-014-1877-0

By:

Tian, Bailing;
Fan, Wenru;
Zong, Qun

Publication type:

Article

Development and Ground Combustion Test of a Subscale Reusable Winged Rocket.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1

By:

Kyoshiro ITAKURA;
Gaku SASAKI;
Shintaro MIYAMOTO;
Hiroshi YAMASAKI;
Takaaki MATSUMOTO;
Koichi YONEMOTO

Publication type:

Article

Development of Main Propulsion System for Reusable Sounding Rocket: Design Considerations and Technology Demonstration.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1

By:

Masaki SATO;
Tomoyuki HASHIMOTO;
Satoshi TAKADA;
Toshiya KIMURA;
Takuo ONODERA;
Yoshihiro NARUO;
Tsuyoshi YAGISHITA;
Ken-ichi NIU;
Takao KANEKO;
Kimihito OBASE

Publication type:

Article

NASA approves new design for shuttle external tank fitting.

Published in:: Advanced Materials & Processes, 2004, v. 162, n. 9, p. 31
Publication type:: Article

MATERIALS for Air and Space.

Published in:: Advanced Materials & Processes, 2000, v. 158, n. 3, p. 63
Publication type:: Article

Committing to the Shuttle Without Ever Having a National Policy.

Published in:

Air Power History, 2005, v. 52, n. 3, p. 36

By:

Temple III, L. Parker

Publication type:

Article