Venturestar™ single stage to orbit reusable launch vehicle program overview

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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Single stage and thrust augmented reusable launch vehicle stability and performance study

10.1063/1.54716 ◽

1998 ◽

Author(s):

Pamela A. Tanck ◽

Kimberly B. Steadman

Keyword(s):

Launch Vehicle ◽

Single Stage ◽

Vehicle Stability ◽

Performance Study ◽

Reusable Launch Vehicle ◽

And Performance

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Life Cycle Analysis of a Single Stage to Orbit (SSTO) Reusable Launch Vehicle

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2003-5264 ◽

2003 ◽

Author(s):

J. Robinson ◽

G. Culver ◽

R. Bishop ◽

E. Bright

Keyword(s):

Life Cycle ◽

Life Cycle Analysis ◽

Launch Vehicle ◽

Single Stage ◽

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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Merits of full flow vs. conventional staged combustion cycles for reusable launch vehicle propulsion

10.1063/1.49964 ◽

1996 ◽

Author(s):

Steven D. Peery ◽

Randy C. Parsley

Keyword(s):

Launch Vehicle ◽

Staged Combustion ◽

Vehicle Propulsion ◽

Reusable Launch Vehicle

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Finite-time attitude tracking control design for reusable launch vehicle in reentry phase based on disturbance observer

Advances in Mechanical Engineering ◽

10.1177/1687814017744077 ◽

2017 ◽

Vol 9 (12) ◽

pp. 168781401774407 ◽

Cited By ~ 1

Author(s):

Fang Wang ◽

Qin Zou ◽

Changchun Hua ◽

Qun Zong

Keyword(s):

Finite Time ◽

Tracking Control ◽

Disturbance Observer ◽

Control Design ◽

Launch Vehicle ◽

Reusable Launch Vehicle ◽

Attitude Tracking ◽

Attitude Tracking Control

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