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HPH.COM

Helicon plasma hydrazine combined micro

Informazioni Generali

Coordinatore:
UNIV. PADOVA (Italia)
Responsabile:
STRANGIO CARMELA - (FRASCATI)
Ruolo ENEA:
PARTNER
Sito WEB:
Sito WEB non disponibile

Programmi Europei

Programma:
Settimo Programma Quadro R&ST (2007-2013) -> SPAZIO (2007-2013) (CP - Progetto di collaborazione)

Descrizione e Attività

Descrizione Generale

The objective of the research program is to design, optimize and develop a space plasma thruster based on helicon-radio-frequency technology and its application to a nano-satellite for attitude and position control. Moreover a detailed feasibility study will be also conducted to evaluate the possibility of using the plasma thruster to heat and decompose a secondary propellant. The feasibility study will asses the possibility of building up a combined-two-mode-thruster able to operate in the low-thrust high-efficiency plasma-mode and high-thrust low-efficiency secondary-propellant-plasma-enhanced mode. Only the plasma thruster will be developed and fully tested during this study. The main characteristics of the thruster are: Power 50 W Weight within 1.5 kg Thrust >1.5 mN Specific Impulse (Isp) >1200 s.

The program will develop thought the following steps:
- Deep numerical-theoretical investigation through dedicated plasma-simulation tools.
- Extensive experimental campaign to validate codes, to investigate the physics phenomena involved and to proof thruster performance.
- The development of a thruster-prototype to be mounted on board of a mini-satellite to demonstrate technology feasibility,
-The study of all the critical issues related to the application to a mini-satellite
- the design and manufacturing of the mini-satellite mock up including all critical components
- analysis of scaling law to lower and higher power.
As a final results of the project, a detailed analysis will be conducted in order to evaluate the possible application of the thruster in space missions requiring low thrust accurate attitude and position control.

Attività svolta da ENEA

Progettazione delle diagnostiche indispensabili per lo studio della fisica dei processi che avvengono nei motori al plasma sia delle antenne di accoppiamento della RF (riscaldamento a radiofrequenza) ai plasmi (gas ionizzato)

Dati Finanziari (in euro)

Costo Eleggibile

Progetto:
4.900.000,00
ENEA:
396.000,00

Contributo

Progetto:
3.570.000,00
ENEA:
300.000,00

Durata del Progetto

Anno di stipula e Durata:
2008 - 36 mesi
Periodo:
01-12-2008 -> 30-11-2011

Partner (15)

Ruolo Nome Nazione
ROVSING A/S Danimarca
CNRS - FRENCH NATIONAL CENTRE FOR SCIENTIFIC RESEARCH Francia
LMS IMAGINE SA Francia
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES Francia
STUDIO PROGETTAZIONE E REALIZZAZIONE DI APPARATI ELETTRONICI DI SELMO ANTONIO Italia
THALES ALENIA SPACE ITALIA SPA Italia
UNIV. BOLOGNA ALMA MATER STUDIORUM (UNIBO) Italia
UNIV. ROMA LA SAPIENZA (UNIROMA1) Italia
AOES GROUP BV - ADVANCED OPERATIONS AND ENGINEERING SERVICES GROUP BV Paesi Bassi
BRADFORD ENGINEERING BV Paesi Bassi
KELDYSH INSTITUTE OF APPLIED MATHEMATICS OF THE RAS Russia
UNIV. POLITECNICA MADRID Spagna
UNIV. KHARKIV Ucraina
COORD UNIV. PADOVA Italia
PARTNER ENEA Italia

Keyword CORDIS (2)

Keyword Argomento
AEROSPACE TECHNOLOGY Industry and technology
SCIENTIFIC RESEARCH RTD Horizontal Topics

Altre Keyword (4)

Keyword
Helicon-radio-frequency
Plasma
Radiofrequency
Space and satellite research