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Tesi etd-02022017-151302


Tipo di tesi
Tesi di laurea magistrale
Autore
AVANZI, FRANCESCO
Indirizzo email
avanzi.francesco.88@gmail.com
URN
etd-02022017-151302
Titolo
0.7 kW Arcjet System Using Green Propellants
Struttura
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Commissione
relatore Prof. Paganucci, Fabrizio
Parole chiave
  • hydrazine
  • green propellant
  • arcjet
Data inizio appello
21/02/2017;
Disponibilità
parziale
Riassunto analitico
Many research programs are focusing the attention on green propellants. Many advantages are associated with their use, in particular the cost reduction. This thesis discusses the implementation of the ADN-based propellant, LMP-103S, on the Arcjet system. Although hydrazine is well used as propellant, it is high in toxicity and difficult for handling. A simple numerical model, developed for this thesis, predicts lower LMP-103S performance than hydrazine in low-power Arcjet systems. The main operative problems of Arcjet thruster relates to erosion, the possible solutions are discussed and the design of a preliminary engineering model is done. The revision on the Arcjet technology and systems reveals that the gas generator and the thruster unit are not mature for the implementation of LMP-103S in the Arcjet system.
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