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SPAce exploration Research for Throttleable Advanced eNgine

Objective

The SPARTAN research aims at developing a throttable propulsion technology, which is mandatorily needed for any planetary soft and precision landing. It relies on the hybrid engine technology, exploiting its capability of being throttled and its proper performances.
This research is complementary to ESA TRP and Piedmont Regional development programs. It implements and strengthens the technological base in view of the future robotics and manned space exploration missions.
The outcomes from the SPARTAN development can be reflected also in many other Earth/Space civilian applications, exploiting both the throttling capability of the propulsion system and the peculiar characteristics of the hybrid engine technology, like: safety, minimum environmental impact (green propellants), lower life cycle costs, responsiveness, competitive Performances, increased reliability, soft ignition and shutdown. The hybrid propulsion system is formed by two major constitutors: the engine itself, housing the fuel, and the oxidizer injection system.
The research focuses on three major objectives, needed to achieve the soft and precision landing capabilities:
 The engine design, specific for throttling functionality
 The oxidizer throttable device development
 The design of the landing case: test bench and testing procedures
Development will be supported by establishing an advanced coding, enabling the definition of the fuel and the throttling behavior of the hybrid engine. Engine definition will be supported by development tests: cold injection case on subscale model, dedicated to the throttling device, and hot firing on lab model, merging the throttling device and the engine model.
In parallel a landing test and associated landing model (flying test bed) will be developed, providing for proven landing model and landing test capabilities. These capabilities will allow demonstrating the soft landing features of a throttable hybrid propulsion technology.

Call for proposal

FP7-SPACE-2010-1
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Coordinator

THALES ALENIA SPACE ITALIA SPA
Address
Via Saccomuro 24
00131 Roma
Italy

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Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
Enrico Gaia (Mr.)
EU contribution
€ 383 569,70

Participants (7)

UNIVERSITA DEGLI STUDI DI PADOVA
Italy
EU contribution
€ 295 467,40
Address
Via 8 Febbraio 2
35122 Padova

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Activity type
Higher or Secondary Education Establishments
Administrative Contact
Sandra Dal Bianco (Ms.)
NAMMO RAUFOSS AS
Norway
EU contribution
€ 364 490,40
Address
Enggata 37
2830 Raufoss

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Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
Jan-Erik Rønningen (Mr.)
BRADFORD ENGINEERING BV
Netherlands
EU contribution
€ 271 589
Address
De Wijper 26
4726 TG Heerle

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Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
Mariol Wildeman (Ms.)
VYSOKE UCENI TECHNICKE V BRNE
Czechia
EU contribution
€ 160 550
Address
Antoninska 548/1
601 90 Brno Stred

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Activity type
Higher or Secondary Education Establishments
Administrative Contact
Antonin Pistek (Prof.)
POLITECNICO DI MILANO
Italy
EU contribution
€ 85 034,50
Address
Piazza Leonardo Da Vinci 32
20133 Milano

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Activity type
Higher or Secondary Education Establishments
Administrative Contact
Fulvio Mongilardi (Mr.)
GMV AEROSPACE AND DEFENCE SA
Spain
EU contribution
€ 241 989,50
Address
Calle Isaac Newton Parque Tecnologico De Madrid
28760 Tres Cantos

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Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
Mariella Graziano (Mrs.)
STUDIEL
France
EU contribution
€ 123 940,75
Address
Avenue Docteur Lefebvre 1027
06271 Villeneuve Loubet

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Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Administrative Contact
David Garbarino (Mr.)