The SPARTAN project exploits both the throttling capability of the propulsion system and the peculiar characteristics of hybrid engine technology. The development includes the establishment of an advanced coding capability, enabling the definition of the fuel and the throttling behaviour of the hybrid engine. The Hybrid propulsion technology has been selected, because to its peculiarities (safety, minimum environmental impact (green propellants), low life cycle costs, responsiveness, competitive performances and increased reliability).

More information could be found here: http://www.spartanproject.eu/.

Description in English
The SPARTAN project exploits both the throttling capability of the propulsion system and the peculiar characteristics of hybrid engine technology. The development includes the establishment of an advanced coding capability, enabling the definition of the fuel and the throttling behaviour of the hybrid engine. The Hybrid propulsion technology has been selected, because to its peculiarities (safety, minimum environmental impact (green propellants), low life cycle costs, responsiveness, competitive performances and increased reliability).

More information could be found here: http://www.spartanproject.eu/.

Keywords
space, exploration, engine, hybrid pulsion, throttling technology

Key words in English
space, exploration, engine, hybrid pulsion, throttling technology

FP7-SPACE-2010-1 262837

Czech

Píštěk Antonín, prof. Ing., CSc. - principal person responsible

Institute of Aerospace Engineering
- responsible department (1.1.1989 - not assigned)
Institute of Aerospace Engineering
- beneficiary (1.2.2011 - 28.2.2013)

PEJCHAR, J.; DANIEL, M.; POPELA, R. Mars probe soft landing test in the Earth conditions. Engineering mechanics 2015 - Extended abstracts. 21st International conference May 11-14, 2015, Svratka, Czech Republic. Extended abstracts. Česká republika: Academy of Sciences of the Czech Republic, v.v.i., 2015. p. 226-227. ISBN: 978-80-86246-42-0.
Detail

PEJCHAR, J.; HÁJEK, T. Modern methods of parachute rescue system testing. In 24th International Conference ENGINEERING MECHANIC 2018. Engineering Mechanics .... Svratka, ČR: 2018. p. 665-669. ISBN: 978-80-86246-88-8. ISSN: 1805-8256.
Detail

FAENZA, M.; MORETTO, F.; TIJSTERMAN, R.; DVOŘÁK, P.; POPELA, R.; PETRONIO, D.; PAVARIN, D. Experimental Characterization of a Cavitating Pintle Valve with H2O2. In Space Propulsion Conference 2014 Proceedings. Paris, France: Space Propulsion Comitee/AAAF, 2014. p. 1-7. ISBN: 978-85-86686-70-2.
Detail

PEJCHAR, J.; DANIEL, M.; POPELA, R. Mars probe soft landing test in the Earth conditions. Svratka, ČR: 2015.
Detail

PEJCHAR, J.; DANIEL, M.; POPELA, R. SOFT LANDING TEST OF AN INTERPLANETARY PROBE IN THE EARTH CONDITIONS. In Sborník příspěvků Mezinárodní Masarykovy konference pro doktorandy a mladé vědecké pracovníky 2014. Hradec králové: MAGNANIMITA. 5. vyd. 2014. ISBN 978-80-87952-07-8, ETTN 042-14-14030-12-4. 2014. Hradec Kralové: MAGNANIMITAS, 2014. p. 1-10. ISBN: 978-80-87952-07-8.
Detail

Responsibility: Píštěk Antonín, prof. Ing., CSc.