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Launch Cost Reduction by Reusing Launch Vehicles

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17EG3106

Subject Category: Research and Development

PDF available here

  • Responsible Representative: Koichi Okita, Research Unit IV, Research and Development Directorate
  • Contact Information: Yoshiki Takama takama.yoshiki@jaxa.jp
  • Members: Yoshiki Takama, Yoshihisa Aoki

Abstract

This research conducts the study of key technologies applied to future reusable launch vehicles including long-life rocket engines, lightweight structures, landing guidance, and small experimental vehicles to validate the technologies.

Reference URL

N/A

Reasons for using JSS2

JSS2 is nessesary for the estimation of aerodynamic performance for a small experimental vehicle.

Achievements of the Year

CFD in the rocket launch phase was conducted as follows:

1) the inside of the rocket nozzle was not calculated.

2) the static pressure, static temperature, and velocity at the nozzle exit were given as the boundary condition.

The calculation started from the first-order accuracy with the pressure at the nozzle exit one third of the nominal value. The calculation was gradually accelerated, and successfully converged at the second-order accuracy with the pressure of the nozzle exit the nominal value.

The axial velocity distribution in the vicinity of the nozzle exit is shown in (Fig. 1). Mach number is 0.1. The angle of attack is 0 deg.

Annual Reoprt Figures for 2017

Fig.1: Axial velocity distribution at the lift-off (M=0.1, AOA=0deg)

 

Publications

N/A

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: N/A
  • Number of Processes: 96
  • Elapsed Time per Case: 300.00 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.23

 

Details

Please refer to System Configuration of JSS2 for the system configuration and major specifications of JSS2.

Computational Resources
System Name Amount of Core Time
(core x hours)
Fraction of Usage*2(%)
SORA-MA 1,895,520.26 0.25
SORA-PP 113.88 0.00
SORA-LM 0.00 0.00
SORA-TPP 0.00 0.00

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 037.71 0.03
/data 889.02 0.02
/ltmp 634.77 0.05

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 0.00 0.00

*1: Fraction of Usage in Total Resources: Weighted average of three resource types (Computing, File System, and Archiver).

*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.

JAXA Supercomputer System Annual Report April 2017-March 2018


ここは、サイドバー・エリアの先頭です。

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Language / 言語

"Annual Report" available

How to use JSS3

To use JSS3, please refer to "How to use JSS3" page .

Location

Chofu Aerospace Center
7-44-1 Jindaiji Higashi-machi, Chofu-shi, Tokyo