scholarly journals Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine for Scientific Observation Using Design Informatics

2013 ◽  
Vol 6 (1) ◽  
pp. 15-27 ◽  
Author(s):  
Kazuhisa CHIBA ◽  
Masahiro KANAZAKI ◽  
Masaki NAKAMIYA ◽  
Koki KITAGAWA ◽  
Toru SHIMADA
Keyword(s):  
Conceptual Design ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Single Stage ◽  
Hybrid Rocket ◽  
Scientific Observation ◽  
Hybrid Rocket Engine

scholarly journals Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics

2014 ◽  
Vol 80 (818) ◽  
pp. TRANS0287-TRANS0287
Author(s):  
Kazuhisa CHIBA ◽  
Shin'ya WATANABE ◽  
Masahiro KANAZAKI ◽  
Koki KITAGAWA ◽  
Toru SHIMADA
Keyword(s):  
Conceptual Design ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Single Stage ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

1109 Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine Using Design Informatics

2013 ◽  
Vol 2013.23 (0) ◽  
pp. _1109-1_-_1109-10_
Author(s):  
Kazuhisa Chiba ◽  
Masahiro Kanazaki ◽  
Koki Kitagawa ◽  
Toru Shimada
Keyword(s):  
Conceptual Design ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Single Stage ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

scholarly journals Structurisation and visualisation of design space for launch vehicle with hybrid rocket engine

2016 ◽  
Vol 2 (1/2) ◽  
pp. 26
Author(s):  
Kazuhisa Chiba ◽  
Masahiro Kanazaki ◽  
N.A. Shin' ◽  
ya Watanabe ◽  
Koki Kitagawa ◽  
...  
Keyword(s):  
Design Space ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

Optimal design for hybrid rocket engine for air launch vehicle

2008 ◽  
Vol 22 (8) ◽  
pp. 1576-1585 ◽  
Author(s):  
Ihnseok Rhee ◽  
Changjin Lee ◽  
Jae-Woo Lee
Keyword(s):  
Optimal Design ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

Conceptual design of a hybrid rocket engine utilizing lunar-derived propellants

1990 ◽  
Author(s):  
D. BROWER ◽  
W. ADAMS ◽  
T. KELLY ◽  
C. EWING ◽  
T. WIERSEMA
Keyword(s):  
Conceptual Design ◽  
Rocket Engine ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine

Multidisciplinary Design Exploration for Sounding Launch Vehicle using Hybrid Rocket Engine in View of Ballistic Performance

2015 ◽  
Vol 32 (3) ◽  
Author(s):  
Kazuhisa Chiba ◽  
Masahiro Kanazaki ◽  
Atthaphon Ariyarit ◽  
Hideyuki Yoda ◽  
Shoma Ito ◽  
...  
Keyword(s):  
Initial Conditions ◽  
Rocket Engine ◽  
Launch Vehicle ◽  
Test Design ◽  
Objective Functions ◽  
Hybrid Rocket ◽  
Ballistic Performance ◽  
Design Problems ◽  
Design Variables ◽  
Hybrid Rocket Engine

AbstractConceptual design of a launch vehicle with a hybrid rocket engine (HRE) has been implemented using design informatics approach in order to investigate the feasibility of a single-stage hybrid rocket. Two test design problems were formulated by using two objective functions: maximization of downrange and minimization of initial gross weight, seven design variables which describe geometry and initial conditions, and one constraint relative to target altitude. The optimization result reveals the economical performance of hybrid rocket is limited with HRE in terms of the maximum downrange achievable. Moreover, the data-mining result indicates the mechanism of design-variable behavior.

scholarly journals Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine

2014 ◽  
Vol 8 (3) ◽  
pp. JAMDSM0023-JAMDSM0023 ◽  
Author(s):  
Kazuhisa CHIBA ◽  
Masahiro KANAZAKI ◽  
Masaki NAKAMIYA ◽  
Koki KITAGAWA ◽  
Toru SHIMADA
Keyword(s):  
Rocket Engine ◽  
Launch Vehicle ◽  
Design Knowledge ◽  
Hybrid Rocket ◽  
Hybrid Rocket Engine
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