Earth Orbital Mission Requirements for Secondary Propulsion Systems and Their Impact on Colloid Systems

1970 ◽  
Vol 92 (3) ◽  
pp. 621-627 ◽  
Author(s):  
Ralph A. Benson

This paper develops the earth synchronous orbital mission requirements for secondary propulsion subsystems (SPS) involving positioning of satellites in orbit and station keeping when in position. It also discusses the orbital requirements associated with attitude control and touches on the requirements for SPS pulsing, thrust vector alignment, and thrust vector control. After developing the earth-orbital mission requirements for SPS, the implications of using low-thrust colloid SPS are discussed. Conclusions are then presented regarding use of colloid, SPS for synchronous earth-orbital operations.

2021 ◽  
Vol 2094 (4) ◽  
pp. 042081
Author(s):  
N A Brykov ◽  
V Yu Kaun ◽  
A A Yatsenko

Abstract The ability to change the magnitude and direction of the thrust vector is a fundamental parameter of the propulsion systems of aircraft. A wide range of methods for controlling these quantities has been developed, which are used depending on the design schemes. The article discusses the organization of the gas-dynamic method of thrust vector control, carried out using distributed gas injection through a porous insert.


2016 ◽  
Vol 49 (17) ◽  
pp. 468-473 ◽  
Author(s):  
Timo Wekerle ◽  
Euler Gonçalves Barbosa ◽  
César Moura Batagini ◽  
Luís E.V. Loures da Costa ◽  
Luís Gonzaga Trabasso

Author(s):  
B. Chandra Mohan Naik ◽  
Praveen Kumar Balguri ◽  
D. Govardhan ◽  
Kavati Aakaanksha

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