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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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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Multi-Objective Multidisciplinary Design Optimization Approach for Partially Reusable Launch Vehicle Design

Journal of Spacecraft and Rockets ◽

10.2514/1.a34601 ◽

2020 ◽

Vol 57 (2) ◽

pp. 373-390

Author(s):

Loic Brevault ◽

Mathieu Balesdent ◽

Ali Hebbal

Keyword(s):

Design Optimization ◽

Multidisciplinary Design Optimization ◽

Launch Vehicle ◽

Multidisciplinary Design ◽

Vehicle Design ◽

Optimization Approach ◽

Multi Objective ◽

Reusable Launch Vehicle ◽

Launch Vehicle Design

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Multidisciplinary Design Optimization of a Two-Stage-to-Orbit Reusable Launch Vehicle with Ethanol-Fueled Rocket-Based Combined Cycle Engines

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ◽

10.2322/tjsass.60.265 ◽

2017 ◽

Vol 60 (5) ◽

pp. 265-275 ◽

Cited By ~ 1

Author(s):

Takahiro FUJIKAWA ◽

Takeshi TSUCHIYA ◽

Sadatake TOMIOKA

Keyword(s):

Design Optimization ◽

Multidisciplinary Design Optimization ◽

Launch Vehicle ◽

Combined Cycle ◽

Multidisciplinary Design ◽

Two Stage ◽

Reusable Launch Vehicle

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Full-stage Reentry Trajectory Optimization for Reusable Launch Vehicle

2020 39th Chinese Control Conference (CCC) ◽

10.23919/ccc50068.2020.9188640 ◽

2020 ◽

Author(s):

Siyuan Wu ◽

Bailing Tian ◽

Zhiyu Li

Keyword(s):

Trajectory Optimization ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Reentry Trajectory ◽

Reentry Trajectory Optimization

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Multidisciplinary Design Optimization for a Reusable Launch Vehicle Using Multiple-Phase Pseudospectral Optimization

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA ◽

10.2514/6.2012-1350 ◽

2012 ◽

Cited By ~ 3

Author(s):

Ryan Carr ◽

Timothy Jorris ◽

Eric Paulson

Keyword(s):

Design Optimization ◽

Multidisciplinary Design Optimization ◽

Launch Vehicle ◽

Multidisciplinary Design ◽

Multiple Phase ◽

Reusable Launch Vehicle

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Approach and landing trajectory optimization for reusable launch vehicle using adaptive Gauss pseudo-spectral method

2017 36th Chinese Control Conference (CCC) ◽

10.23919/chicc.2017.8027798 ◽

2017 ◽

Author(s):

Chaofan Zhang ◽

Qun Zong ◽

Qi Dong ◽

Bailing Tian ◽

Zhiyu Li ◽

...

Keyword(s):

Spectral Method ◽

Trajectory Optimization ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Pseudo Spectral Method ◽

Pseudo Spectral ◽

Landing Trajectory

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Optimisation of a reusable launch vehicle concept

10.2514/6.2000-4180 ◽

2000 ◽

Author(s):

M. Tetlow ◽

U. Schoettle ◽

G. Schneider

Keyword(s):

Launch Vehicle ◽

Vehicle Concept ◽

Reusable Launch Vehicle

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A hybrid parallel Harris hawks optimization algorithm for reusable launch vehicle reentry trajectory optimization with no-fly zones

Soft Computing ◽

10.1007/s00500-021-06039-y ◽

2021 ◽

Author(s):

Ya Su ◽

Ying Dai ◽

Yi Liu

Keyword(s):

Optimization Algorithm ◽

Trajectory Optimization ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Reentry Trajectory ◽

Reentry Trajectory Optimization

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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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