RESISTOJET propulsion system for small satellite

Darfilal Djamal; Khatir Mohamed; Alim Rustem Aslan

doi:10.1109/RAST.2019.8767847

RESISTOJET propulsion system for small satellite

Darfilal Djamal
, Khatir Mohamed
, Alim Rustem Aslan

Uzay Mühendisliği Bölümü

Algerian Space Agency
Algerian Space AgencyASAL

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

13 Atıf (Scopus)

Özet

Due to the launch safety constraints placed on Space companies built microsatellites, designing a simple and reliable propulsion system with performance and characteristics in line with the typical requirements of microsatellites presents a significant challenge to aspiring engineers. This paper presents the design process of a low-cost, propulsion system with a two-phase high density propellant. The aim of this study is the preliminary design of a 50mN RESISTOJET system operating at low pressure. The preliminary design and the optimization of the thruster dimensions are presented.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019
Editörler	S. Menekay, O. Cetin, O. Alparslan
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	159-166
Sayfa sayısı	8
ISBN (Elektronik)	9781538694480
DOI'lar	https://doi.org/10.1109/RAST.2019.8767847
Yayın durumu	Yayınlandı - Haz 2019
Etkinlik	9th International Conference on Recent Advances in Space Technologies, RAST 2019 - Istanbul, Türkiye Süre: 11 Haz 2019 → 14 Haz 2019

Yayın serisi

Adı	Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	9th International Conference on Recent Advances in Space Technologies, RAST 2019
Ülke/Bölge	Türkiye
Şehir	Istanbul
Periyot	11/06/19 → 14/06/19

Bibliyografik not

Publisher Copyright:
© 2019 IEEE.

Belgeye Erişim

10.1109/RAST.2019.8767847

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Djamal, D., Mohamed, K., & Rustem Aslan, A. (2019). RESISTOJET propulsion system for small satellite. In S. Menekay, O. Cetin, & O. Alparslan (Eds.), Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019 (pp. 159-166). Makale 8767847 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2019.8767847

Djamal, Darfilal ; Mohamed, Khatir ; Rustem Aslan, Alim. / RESISTOJET propulsion system for small satellite. Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. editör / S. Menekay ; O. Cetin ; O. Alparslan. Institute of Electrical and Electronics Engineers Inc., 2019. pp. 159-166 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019).

@inproceedings{953c4f3caf0f4025ab60f875d1f095bf,

title = "RESISTOJET propulsion system for small satellite",

abstract = "Due to the launch safety constraints placed on Space companies built microsatellites, designing a simple and reliable propulsion system with performance and characteristics in line with the typical requirements of microsatellites presents a significant challenge to aspiring engineers. This paper presents the design process of a low-cost, propulsion system with a two-phase high density propellant. The aim of this study is the preliminary design of a 50mN RESISTOJET system operating at low pressure. The preliminary design and the optimization of the thruster dimensions are presented.",

keywords = "Cold gas, heater, RESISTOJET, small satellites",

author = "Darfilal Djamal and Khatir Mohamed and \{Rustem Aslan\}, Alim",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 9th International Conference on Recent Advances in Space Technologies, RAST 2019 ; Conference date: 11-06-2019 Through 14-06-2019",

year = "2019",

month = jun,

doi = "10.1109/RAST.2019.8767847",

language = "English",

series = "Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "159--166",

editor = "S. Menekay and O. Cetin and O. Alparslan",

booktitle = "Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019",

address = "United States",

}

Djamal, D, Mohamed, K & Rustem Aslan, A 2019, RESISTOJET propulsion system for small satellite. in S Menekay, O Cetin & O Alparslan (eds), Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019., 8767847, Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019, Institute of Electrical and Electronics Engineers Inc., pp. 159-166, 9th International Conference on Recent Advances in Space Technologies, RAST 2019, Istanbul, Türkiye, 11/06/19. https://doi.org/10.1109/RAST.2019.8767847

RESISTOJET propulsion system for small satellite. / Djamal, Darfilal; Mohamed, Khatir; Rustem Aslan, Alim.
Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. ed. / S. Menekay; O. Cetin; O. Alparslan. Institute of Electrical and Electronics Engineers Inc., 2019. p. 159-166 8767847 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - RESISTOJET propulsion system for small satellite

AU - Djamal, Darfilal

AU - Mohamed, Khatir

AU - Rustem Aslan, Alim

PY - 2019/6

Y1 - 2019/6

N2 - Due to the launch safety constraints placed on Space companies built microsatellites, designing a simple and reliable propulsion system with performance and characteristics in line with the typical requirements of microsatellites presents a significant challenge to aspiring engineers. This paper presents the design process of a low-cost, propulsion system with a two-phase high density propellant. The aim of this study is the preliminary design of a 50mN RESISTOJET system operating at low pressure. The preliminary design and the optimization of the thruster dimensions are presented.

AB - Due to the launch safety constraints placed on Space companies built microsatellites, designing a simple and reliable propulsion system with performance and characteristics in line with the typical requirements of microsatellites presents a significant challenge to aspiring engineers. This paper presents the design process of a low-cost, propulsion system with a two-phase high density propellant. The aim of this study is the preliminary design of a 50mN RESISTOJET system operating at low pressure. The preliminary design and the optimization of the thruster dimensions are presented.

KW - Cold gas

KW - heater

KW - RESISTOJET

KW - small satellites

UR - https://www.scopus.com/pages/publications/85073908368

U2 - 10.1109/RAST.2019.8767847

DO - 10.1109/RAST.2019.8767847

M3 - Conference contribution

AN - SCOPUS:85073908368

T3 - Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

SP - 159

EP - 166

BT - Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

A2 - Menekay, S.

A2 - Cetin, O.

A2 - Alparslan, O.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 9th International Conference on Recent Advances in Space Technologies, RAST 2019

Y2 - 11 June 2019 through 14 June 2019

ER -

Djamal D, Mohamed K, Rustem Aslan A. RESISTOJET propulsion system for small satellite. In Menekay S, Cetin O, Alparslan O, editörler, Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. Institute of Electrical and Electronics Engineers Inc. 2019. p. 159-166. 8767847. (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019). doi: 10.1109/RAST.2019.8767847

RESISTOJET propulsion system for small satellite

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Yayın serisi

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Bibliyografik not

Belgeye Erişim

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