Precision Measurement of Erosive Burning Effect in a Small Solid Propellant Motor by Use of X-ray Absorption Diagnostics
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- Hasegawa Hiroshi
- 東海大学大学院工学研究科航空宇宙学専攻
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- Tokudome Shin-ichiro
- 文部科学省宇宙科学研究所
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- Hanzawa Masahisa
- 東海大学工学部航空宇宙学科
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- Kohno Masahiro
- 文部科学省宇宙科学研究所
Bibliographic Information
- Other Title
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- X線透過法による小型固体モータにおける侵食燃焼効果の精密測定
- Xセン トウカホウ ニ ヨル コガタ コタイ モータ ニ オケル シンショク ネンショウ コウカ ノ セイミツ ソクテイ
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Abstract
The erosive burning effects in a small test motor loaded with practical composite propellants have been investigated in detail by using an X-ray absorption diagnostics to measure the propellant local regression. The motor was specially designed to have two propellant slabs and was called as DSM (Double Slab Motor). Significant erosive burning was forced to occur in the motor by varying combustion pressure and mass flux in the port. A new simple correlative equation is derived, which predicts accurately not only pressure history but also local regression of burning surface. The equation is characteristic in the non-dimensionalized threshold mass flux and includes the terms to consider both effects of pressure and of motor scale.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 51 (594), 364-370, 2003
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204470597120
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- NII Article ID
- 10011458471
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 6647339
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed