BURN RATE DETERMINATION FROM THE STATIC TEST RESULTS

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Abstract
Solid rocket motor design is an iterative process. As a first step, burn rate coefficients from the strand burner were used for initial motor sizing. Static test is done to measure the performance of rocket motor. Pressure-time trace from static test is used to calculate the burn rate coefficients. The burn rate coefficients calculated from pressure-time trace is considered for performance prediction as well as strand burner burn rate coefficients.
Informasi Detil
Judul Seri -
No. Panggil -
Penerbit Indonesia Book Project : Jakarta.,
Deskripsi Fisik Hlm. 87-94:Il. ; 28 cm.
Bahasa English
ISBN/ISSN 978-602-70353-4-8
Klasifikasi NONE
Edisi Aeronautic and Space Technology....
Subyek Design
Static test
Burn Rate
Solid Rocket Motor,
Performance Prediction
Pernyataan Tanggungjawab
LAPAN
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