The calculation of the thrust of a rocket motor
Traditionally the thrust of a rocket motor is calculated by first calculating the thrust coefficient and then multiplying it by the product of the throat area and pressure. The thrust coefficient is calculated using a standard gas dynamics equation. This equation assumes that the combustion products...
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| Format: | Article |
| Language: | Afrikaans |
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South African Journal of Science and Technology
1993-07-01
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| Series: | South African Journal of Science and Technology |
| Online Access: | http://www.satnt.ac.za/index.php/satnt/article/view/565 |