The design procedure of the aerodynamic maneuver for the fall location changing of the carrier rocket stage

Author

Trushlyakov, V.I. ; Sitnikov, D.V.

Author_Institution

Omsk State Tech. Univ., Omsk, Russia

fYear

2014

fDate

11-13 Nov. 2014

Firstpage

1

Lastpage

4

Abstract

The procedure of the computation of the program trajectory of the spent stage descending to the impact point and stabilization about the program trajectory considered. The requirements to gas-jet-propelled stabilization system and the operating cycle gasification board system for residual fuel used for the stabilization formulated. The stabilization processes calculations, evaluation of displacement spent stage descending location about the initial trajectory for example first stage separable part of the carrier rocket "Soyuz-2.1.v" at various descending trajectory synthesis schemes.

Keywords

aerodynamics; design engineering; mechanical stability; rockets; space vehicles; vehicle dynamics; Soyuz-2.1.v; aerodynamic maneuver design procedure; carrier rocket stage; descending trajectory synthesis schemes; displacement spent stage descending location; fall location changes; gas-jet-propelled stabilization system; impact point; operating cycle gasification board system; program trajectory; residual fuel; Aerodynamics; Force; Rockets; Torque; Trajectory; Vehicles; the impact area square; the motion control system; the spent stage; the stabilization system;

fLanguage

English

Publisher

ieee

Conference_Titel

Dynamics of Systems, Mechanisms and Machines (Dynamics), 2014

Conference_Location

Omsk

Print_ISBN

978-1-4799-6406-2

Type

conf

DOI

10.1109/Dynamics.2014.7005700

Filename

7005700