本文へ移動

サイトナビゲーションへ移動

検索ボックスへ移動

サイドバーへ移動

ここは、本文エリアの先頭です。

Numerical Simulations for H3 Rocket Development

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17EK2302

Subject Category: Space Technology

PDF available here

  • Responsible Representative: Masashi Okada, Space Technology Directorate, H3 Project Team
  • Contact Information: Hideyo Negishi negishi.hideyo@jaxa.jp
  • Members: Seiji Tsutsumi, Masashi Kanamori, Hiroaki Amakawa, Masaaki Ino, Hironori Fujiwara, Masaharu Abe, Hiroyuki Ito, Shinji Ohno, Takenori Nakajima, Hideyo Negishi, Yu Daimon, Takanori Haga, Taro Shimizu, Junya Aono, Tetsufumi Ohmaru

Abstract

Please refer to the following URL: http://global.jaxa.jp/projects/rockets/h3/

Reference URL

Please refer to 'JAXA | H3 Launch Vehicle'.

Reasons for using JSS2

Risk management is the key to make a success of a large-scale development project like H3 rocket. This is because its development schedule and cost could be significantly influenced by the face of imminent risks when new technologies are under system-level verification and validation. In order to complete the project under defined period and cost, a variety of efforts are essential for planning and process of technology development itself in terms of efficiency and certainty. In that context, numerical simulation technologies and JSS2 have been playing one of major roles to make the H3 project a success.

Achievements of the Year

With regard to the booster engine, 'LE-9', under detailed design phase, evaluation of design and risks as well as studies for improvement were carried out by making full use of JSS2.

Publications

■ Presentations

1) Funo, Y., et al., "Progress Report of Deatiled Design of H3 rocket," 40th Space Development and Utilization Division of Research and Development Bureau in MEXT(the Ministry of Education, Culture, Sports, Science and Technology), Jan. 24th, 2018.

2) Azuma, N., et al., "Development Status of LE-9 Engine Turbopumps," AIAA Propulsion and Energy Forum, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, G.A., July 10-12, 2017.

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: N/A
  • Number of Processes: 2 - 2500
  • Elapsed Time per Case: 300.00 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 7.19

 

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 60,494,643.13 8.00
SORA-PP 6,871.84 0.09
SORA-LM 220.72 0.11
SORA-TPP 53,598.70 0.29

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 10,303.37 7.14
/data 69,123.46 1.28
/ltmp 5,110.81 0.39

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 104.20 4.48

*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。

News - Recent Posts

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