Numerical Study on Response Characteristics of Solid Rocket Pintle Motor

Numerical Study on Response Characteristics of Solid Rocket Pintle Motor

Show other versions (1)

Pintle technology is currently a versatile technology used in a solid rocket motor (SRM) to control the desired thrust by changing the nozzle throat area, while effectively controlling the chamber pressure at the same time. The sudden movement of the pintle can induce rapid changes in the flow field...

Full description

Bibliographic Details
Main Authors: Jeevan Sapkota, Yi Hua Xu, Hai Jun Sun
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2019-08-01
Series:Journal of Aerospace Technology and Management
Subjects:
SRM
Pintle
Thrust regulation
Online Access:http://www.scielo.br/pdf/jatm/v11/2175-9146-jatm-11-e3419.pdf

Similar Items

Similar Items