Aerospike nozzles are often studied because of their intrinsic self-adaptation behavior to the atmospheric pressure. Another unique feature of aerospike nozzles is their flexible and effective integration with the underlying vehicle. This latter aspect, if fully exploited, could be of interest for both lower stages operating in the atmosphere and for upper stages operating in vacuum. In this paper, a numerical analysis is carried out of the possible advantages of using an aerospike engine for a typical upper stage configuration, discussing basic aspects of aerospike and internal expansion design, clustering and plug truncation length.

Design and evaluation of aerospike nozzles for an upper stage application / Nasuti, Francesco; Fiore, Matteo; Messina, Vincenzo; Valeriani, Alessio; Bianchi, Daniele. - (2024). (Intervento presentato al convegno 7th edition of the Space Propulsion Conference SP2020+1 tenutosi a Online virtual conference).

Design and evaluation of aerospike nozzles for an upper stage application

Francesco Nasuti
Writing – Review & Editing
;
Matteo Fiore
Writing – Original Draft Preparation
;
Vincenzo Messina
Writing – Original Draft Preparation
;
Alessio Valeriani
Writing – Original Draft Preparation
;
Daniele Bianchi
Writing – Review & Editing
2024

Abstract

Aerospike nozzles are often studied because of their intrinsic self-adaptation behavior to the atmospheric pressure. Another unique feature of aerospike nozzles is their flexible and effective integration with the underlying vehicle. This latter aspect, if fully exploited, could be of interest for both lower stages operating in the atmosphere and for upper stages operating in vacuum. In this paper, a numerical analysis is carried out of the possible advantages of using an aerospike engine for a typical upper stage configuration, discussing basic aspects of aerospike and internal expansion design, clustering and plug truncation length.
2024
7th edition of the Space Propulsion Conference SP2020+1
nozzle; upper stage; aerospike
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Design and evaluation of aerospike nozzles for an upper stage application / Nasuti, Francesco; Fiore, Matteo; Messina, Vincenzo; Valeriani, Alessio; Bianchi, Daniele. - (2024). (Intervento presentato al convegno 7th edition of the Space Propulsion Conference SP2020+1 tenutosi a Online virtual conference).
File allegati a questo prodotto
Non ci sono file associati a questo prodotto.

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1646312
 Attenzione

Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo

Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus ND
  • ???jsp.display-item.citation.isi??? 0
social impact