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First results of PRECISE—Development of a MEMS-based monopropellant micro chemical propulsion system
Autor:
Mikhail Ivanov, Hakan Johansson, Yann Batonneau, Dimitri Telitschkin, Markus Gauer, Ulrich Gotzig, Remco J. Wiegerink, Phil Palmer
Publikováno v:
Acta Astronautica
Acta Astronautica, Elsevier, 2014, 93 pp.77-83. ⟨10.1016/j.actaastro.2013.06.010⟩
Acta astronautica, 93, 77-83. Elsevier
Acta Astronautica, Elsevier, 2014, 93 pp.77-83. ⟨10.1016/j.actaastro.2013.06.010⟩
Acta astronautica, 93, 77-83. Elsevier
International audience; PRECISE focuses on the research and development of a MEMS-based monopropellant micro chemical propulsion system for highly accurate attitude control of satellites. The availability of such propulsion systems forms the basis fo
Autor:
Yann Batonneau, Remco J. Wiegerink, Christopher Brunskill, Ulrich Gotzig, Pelle Rangsten, Klaus Hannemann, Dimitri Telitschkin, Markus Gauer, Mikhail Ivanov
Publikováno v:
Joint Propulsion Conferences: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Joint Propulsion Conferences
Joint Propulsion Conferences
This paper gives an overview on preliminary results of the project PRECISE. PRECISE focuses on the research and development of a MEMS-based monopropellant micro Chemical Propulsion System (μCPS) for highly accurate attitude control of satellites. Sp
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The DLR TAU code is enhanced with the CICSAM method for an algebraic reconstruction of the fluid interface. The incompressible module of the DLR TAU Code is cast in a finite-volume projection method infrastructure for variable density flows. The infr
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The DLR TAU code is enhanced with the volume-of-fluid method (VOF) for a reconstruction of the fluid interface. The compressible Reynolds-Averaged-Navier-Stokes equations are discretized by a finite volume technique using tetrahedra, pyramids, prisms
Autor:
Markus Gauer, Allan Paull
When flying at hypersonic speeds, it is a fundamental requirement to reduce the high drag resulting from a blunt nose cone in the ascent stage to increase the payload weight on the one hand and decrease the amount of energy needed to overcome the Ear
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b7d8a6dcd01bb31d4ce379b5e852152c
https://elib.dlr.de/55615/
https://elib.dlr.de/55615/
Autor:
Mikhail Ivanov, Phil Palmer, Yann Batonneau, Ulrich Gotzig, Dimitri Telitschkin, Hakan Johansson, Markus Gauer, Remco J. Wiegerink
Publikováno v:
Scopus-Elsevier
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012
PRECISE focuses on the research and development of a MEMS-based monopropellant micro Chemical Propulsion System (μCPS) for highly accurate attitude control of satellites. The availability of μCPS forms the basis for defining new mission concepts su
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0fcc9592040e03cb03e9fb75791343ac
http://www.scopus.com/inward/record.url?eid=2-s2.0-84880818317&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84880818317&partnerID=MN8TOARS