Simulation and Analyses of Stage Separation of Two-Stage Reusable Launch Vehicles-Reference-Cited by-同舟云学术

Simulation and Analyses of Stage Separation of Two-Stage Reusable Launch Vehicles

Published:2005-05-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
language:
Short-container-title:

Author:

Pamadi Bandu¹,Neirynck Thomas¹,Hotchko Nathaniel¹,Tartabini Paul¹,Scallion William¹,Murphy Kelly¹,Covell Peter¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3247

Reference26 articles.

1. 1Dillenius, M.F.E., Perkins, S.C., and Nixon, D., Pylon Carriage and Separation of Stores, AIAA Progress in Astronautics andAeronautics:TacticalMissileAerodynamics-GeneralTopics,M.J.Hemsch,ed.,Vol.141,1992.

2. 2Taylor, R.T., and Alford, W. J, Jr., A wind tunnel investigation of the carry loads and mutual interference effects of 1/40- scalemodelsoftheX-15andB-52airplanesincombination,NASATMX-184,December1959.

3. 3Decker, J.P., and Wilhite, A. W., Technology and Methodology of Separating Two Similar Size Aerospace Vehicles Within theAtmosphere.AIAAPaper1975-29,Jan.1975.

4. 4Decker, J. P.,Experimental Aerodynamics and Analysis of the Stage Separation of Reusable Launch Vehicles. NASA-SP148,January1967.

5. 5Decker, J. P., and Gera,J.,An Exploratory Study of Parallel-Stage Separation of Reusable Launch Vehicles. NASA TN D4765,October1968.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis and optimization of an air-launch-to-orbit separation;Acta Astronautica;2015-03

2. Changing law of launching pitching angular velocity of rotating missile;Chinese Journal of Aeronautics;2014-10

3. An Experimenal Study on Booster Configuration of TSTO Type Space Plane for Reduction of Shock Wave Interference;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2013

4. Design optimization for robustness in multiple performance functions;Structural and Multidisciplinary Optimization;2012-12-13

5. Effective fault diagnosis based on strong tracking UKF;Aircraft Engineering and Aerospace Technology;2011-09-06