Integrated optimization for single-stage-to-orbit using a pulse detonation engine

Hiroaki Yoshida, Michael Matthew Micci, Masakatsu Nakane, Katsuhito Yamaguchi, Yoshio Ishikawa

Research output: Contribution to journalArticle

Abstract

A new optimization method, called the stochastic process optimization technique, was developed. The integrated optimization of single-stage-to-orbit vehicles with two different engines systems was achieved. Although the performances of the two engine types were different, similar airframe configurations and flight paths were obtained. Additionally, different flight paths for similar airframe configurations were obtained as temporary optimal solutions during the optimization process. This transition of the optimal solution reveals the relationships between the engine performance, the airframe configuration, and the flight path, on which the integrated optimization is based. It was also found that improving the specific impulse at low Mach numbers may improve the feasibility of single-stage-to-orbit vehicles.

Original languageEnglish (US)
Pages (from-to)983-989
Number of pages7
JournalJournal of Spacecraft and Rockets
Volume56
Issue number4
DOIs
StatePublished - Jan 1 2019

Fingerprint

Pulse detonation engines
pulse detonation engines
engine
Orbits
airframes
flight paths
Flight paths
single stage to orbit vehicles
Airframes
orbits
optimization
engines
flight
Engines
configurations
specific impulse
stochastic processes
stochasticity
Random processes
Mach number

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Yoshida, Hiroaki ; Micci, Michael Matthew ; Nakane, Masakatsu ; Yamaguchi, Katsuhito ; Ishikawa, Yoshio. / Integrated optimization for single-stage-to-orbit using a pulse detonation engine. In: Journal of Spacecraft and Rockets. 2019 ; Vol. 56, No. 4. pp. 983-989.
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Integrated optimization for single-stage-to-orbit using a pulse detonation engine. / Yoshida, Hiroaki; Micci, Michael Matthew; Nakane, Masakatsu; Yamaguchi, Katsuhito; Ishikawa, Yoshio.

In: Journal of Spacecraft and Rockets, Vol. 56, No. 4, 01.01.2019, p. 983-989.

Research output: Contribution to journalArticle

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