Optimisation of a reusable launch vehicle concept

Development Program for An Advanced In-Line Reusable Launch Vehicle Concept Using a Small-scale End-Burning Solid and Hybrid Rocket Glider Demonstrator Approach

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2014-3548 ◽

2014 ◽

Author(s):

Adam J. Baran ◽

Clay M. Blanchard ◽

Preston A. Spyridon ◽

Steven M. Hollander ◽

Sean R. McBride ◽

...

Keyword(s):

Development Program ◽

Launch Vehicle ◽

Small Scale ◽

Vehicle Concept ◽

Hybrid Rocket ◽

Reusable Launch Vehicle

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An In-Line Reusable Launch Vehicle Concept Using Confined Load-Bearing Frozen Propellants

49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2013-3921 ◽

2013 ◽

Author(s):

Adam J. Baran ◽

Michael J. Anderson ◽

Jordan T. Auxt

Keyword(s):

Launch Vehicle ◽

Vehicle Concept ◽

Load Bearing ◽

Reusable Launch Vehicle

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Multidisciplinary Design & Trajectory Optimization of the Reusable Launch Vehicle Concept Hopper

2007 3rd International Conference on Recent Advances in Space Technologies ◽

10.1109/rast.2007.4283979 ◽

2007 ◽

Cited By ~ 1

Author(s):

Osman Kalden

Keyword(s):

Trajectory Optimization ◽

Launch Vehicle ◽

Multidisciplinary Design ◽

Vehicle Concept ◽

Reusable Launch Vehicle

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Aerodynamic characteristics of a single-stage-to-orbit wing body reusable launch vehicle concept

10.2514/6.1996-196 ◽

1996 ◽

Author(s):

Anthony Springer

Keyword(s):

Aerodynamic Characteristics ◽

Launch Vehicle ◽

Single Stage ◽

Vehicle Concept ◽

Reusable Launch Vehicle

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The Triplet Reusable Launch Vehicle Concept

42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2006-4960 ◽

2006 ◽

Author(s):

James Martin

Keyword(s):

Launch Vehicle ◽

Vehicle Concept ◽

Reusable Launch Vehicle

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Second generation reusable launch vehicle servicing of the International Space Station

10.2514/6.2000-5141 ◽

2000 ◽

Author(s):

Janet Letchworth ◽

Gary Letchworth

Keyword(s):

International Space Station ◽

Second Generation ◽

Space Station ◽

Launch Vehicle ◽

International Space ◽

Reusable Launch Vehicle

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Practical Composite Damage Tolerance Approach for Reusable Launch Vehicle Applications

AIAA Scitech 2021 Forum ◽

10.2514/6.2021-1166 ◽

2021 ◽

Author(s):

Vinay K. Goyal ◽

Pavel Babuska ◽

Sahar Maghsoudy-Louyeh ◽

Dhruv Patel

Keyword(s):

Damage Tolerance ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Composite Damage ◽

Tolerance Approach

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Reentry attitude tracking control based on fuzzy feedforward for reusable launch vehicle

International Journal of Control Automation and Systems ◽

10.1007/s12555-009-0401-7 ◽

2009 ◽

Vol 7 (4) ◽

pp. 503-511 ◽

Cited By ~ 30

Author(s):

Yu-Hui Wang ◽

Qing-Xian Wu ◽

Chang-Sheng Jiang ◽

Guo-Yong Huang

Keyword(s):

Tracking Control ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Attitude Tracking ◽

Attitude Tracking Control

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Inverse Optimal Control Via Diagonal Stabilization Applied to Attitude Tracking of a Reusable Launch Vehicle

Journal of Optimization Theory and Applications ◽

10.1007/s10957-021-01831-0 ◽

2021 ◽

Author(s):

Prasanna Parvathy ◽

Jeevamma Jacob

Keyword(s):

Optimal Control ◽

Launch Vehicle ◽

Inverse Optimal Control ◽

Reusable Launch Vehicle ◽

Attitude Tracking

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Integrated Finite-Time Disturbance Observer and Controller Design for Reusable Launch Vehicle in Reentry Phase

Journal of Aerospace Engineering ◽

10.1061/(asce)as.1943-5525.0000670 ◽

2017 ◽

Vol 30 (1) ◽

pp. 04016076 ◽

Cited By ~ 5

Author(s):

Qi Dong ◽

Qun Zong ◽

Bailing Tian ◽

Fang Wang

Keyword(s):

Finite Time ◽

Disturbance Observer ◽

Controller Design ◽

Launch Vehicle ◽

Reusable Launch Vehicle

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