|Table of Contents|

Several foreign rocket engine thrust vector measuring devices(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2021年04期
Page:
6-12
Research Field:
专论与综述
Publishing date:

Info

Title:
Several foreign rocket engine thrust vector measuring devices
Author(s):
LIU Wanlong; WANG Dezhi; LIU Shuo; TIAN Guohua; ZHU Haowei
(Beijing Institute of Aerospace Testing Technology,Beijing 100074, China)
Keywords:
rocket engine thrust vector measuring device
PACS:
V433
DOI:
-
Abstract:
In an ideal state,the rocket engine thrust line of action is coincided with the center axis of the engine.But due to the machining accuracy,the asymmetric flow of high-temperature and high-pressure gas in the nozzle,and the ablation of the nozzle throat,the actual engine thrust line is deviated from the theory thrust line.The rocket engine thrust is a space vector.During the operation of the rocket engine,the size,direction and the application point position of the thrust are constantly changing with time.The flight trajectory of the aircraft is significantly affected by the thrust vector.In view of the need of rocket engine thrust vector measurement,more research on rocket engine thrust vector measurement device had been conducted in the United States and other western countries.However,due to the reason of technical secrecy,the literatures of thrust vector measuring device are relatively few.In this paper,some overseas materials of rocket engine thrust vector measurement device were collected.The basic concept of the thrust vector were introduced in this paper.An overview of the thrust vector measuring device of rocket engine in the United States,Japan,Russia and South Korea was given in this paper,which can be provided as reference for domestic counterparts.

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