Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method

Jeongmoo Huh; Chul Park; Sejin Kwon

Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method

Jeongmoo Huh, Chul Park, Sejin Kwon

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

This paper reports the results of conceptual design of sounding rocket, based on laboratory-scale rocket propulsion technologies. 2,500 N class hydrogen peroxide/polyethylene hybrid propulsion system and 250 N class hydrogen peroxide monopropellant thruster were used for main propulsion and attitude control operations, respectively. The attitude control of the sounding rocket was simulated using developed 6 degree of freedom code and feasibility of the bang-bang attitude control using only one monopropellant thruster for spinning sounding rocket was determined. The attitude control simulation results successfully showed the precession motion of the spinning sounding rocket and practicality of the bang-bang control using one thruster.

Original language	English
Title of host publication	66th International Astronautical Congress 2015, IAC 2015
Subtitle of host publication	Space - The Gateway for Mankind's Future
Publisher	International Astronautical Federation, IAF
Pages	7617-7621
Number of pages	5
ISBN (Electronic)	9781510818934
Publication status	Published - 2015
Externally published	Yes
Event	66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015 - Jerusalem, Israel Duration: Oct 12 2015 → Oct 16 2015

Publication series

Name	Proceedings of the International Astronautical Congress, IAC
Volume	10
ISSN (Print)	0074-1795

Conference

Conference	66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Country/Territory	Israel
City	Jerusalem
Period	10/12/15 → 10/16/15

ASJC Scopus subject areas

Aerospace Engineering
Astronomy and Astrophysics
Space and Planetary Science

Cite this

Huh, J., Park, C., & Kwon, S. (2015). Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method. In 66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future (pp. 7617-7621). (Proceedings of the International Astronautical Congress, IAC; Vol. 10). International Astronautical Federation, IAF.

Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method. / Huh, Jeongmoo; Park, Chul; Kwon, Sejin.
66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future. International Astronautical Federation, IAF, 2015. p. 7617-7621 (Proceedings of the International Astronautical Congress, IAC; Vol. 10).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Huh, J, Park, C & Kwon, S 2015, Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method. in 66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future. Proceedings of the International Astronautical Congress, IAC, vol. 10, International Astronautical Federation, IAF, pp. 7617-7621, 66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015, Jerusalem, Israel, 10/12/15.

Huh, Jeongmoo ; Park, Chul ; Kwon, Sejin. / Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method. 66th International Astronautical Congress 2015, IAC 2015: Space - The Gateway for Mankind's Future. International Astronautical Federation, IAF, 2015. pp. 7617-7621 (Proceedings of the International Astronautical Congress, IAC).

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abstract = "This paper reports the results of conceptual design of sounding rocket, based on laboratory-scale rocket propulsion technologies. 2,500 N class hydrogen peroxide/polyethylene hybrid propulsion system and 250 N class hydrogen peroxide monopropellant thruster were used for main propulsion and attitude control operations, respectively. The attitude control of the sounding rocket was simulated using developed 6 degree of freedom code and feasibility of the bang-bang attitude control using only one monopropellant thruster for spinning sounding rocket was determined. The attitude control simulation results successfully showed the precession motion of the spinning sounding rocket and practicality of the bang-bang control using one thruster.",

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Conceptual design of small scale hybrid sounding rocket and attitude control with bang-bang method

Abstract

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Conference

ASJC Scopus subject areas

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