Improvement of Fuel Regression Rate by Impinging Jet for High Thrust Hybrid Rocket Motors

• NAGATA H.

収録刊行物

• Proceedings of the International Symposium on Space Technology and Science, 2000

  Proceedings of the International Symposium on Space Technology and Science, 2000 2000

詳細情報

• CRID: 1572824500220007552
• NII論文ID: 10018055218
• データソース種別:
  • CiNii Articles