STUDY DESIGN OF SMART FEELING SENSITIVITY BASED ON THE HOMOLOGOUS MODEL USED IN ROCKET ENGINE TESTING

  • Phạm Nhật Quang
  • Nguyễn Thị Lan Hương

Abstract

The paper presents a calculation method for a type of rocket engine thrust
measuring sensor with integrated circuit processing, signal processing. The
results showed that the error between calculation and product within the
permitted range.
điểm /   đánh giá
Published
2019-05-22
Issue
No. 51 (2019)
Section
RESEARCH AND DEVELOPMENT