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2024 | OriginalPaper | Chapter

1. An Overview of Green Propellants and Propulsion System Applications: Merits and Demerits

Authors : Wai Siong Chai, Linlin Liu, Xing Sun, Xinyang Li, Yu-Ying Lu

Published in: Recent Advancements in Green Propulsion

Publisher: Springer Nature Switzerland

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Abstract

Embarking on the space exploration demands propulsion systems that not only push the boundaries of efficiency but also align with the principles of environmental concerns, this chapter offers a comprehensive discussion of their merits and demerits. From the eco-friendly promises of hydroxylammonium nitrate (HAN) and ammonium dinitramide (ADN) to the potential drawbacks of inherent defects and costly raw materials, this chapter navigates the intricate landscape of propellant technologies. The chapter unfolds with a spotlight on the merits of green propellants, emphasizing their role in reducing pollution and enhancing operational safety. The advantages of non-toxic, safe, and environmentally friendly propellants are the focus of this chapter, promising a paradigm shift in propellant technologies. Yet, challenges such as inherent defects, expensive raw materials, and the quest for higher energy performance present challenges that demand innovative solutions. The contrast between green chemical propulsion and non-chemical propulsion systems becomes apparent as the discussion widens to the propulsion systems. Despite their maturity, solid propulsion systems grapple with limitations in control and safety. In contrast, the promise of electric, solar, and nuclear systems remains on the horizon, with technical issues remaining unsolved. The chapter concludes with a call to action for the future of space propulsion technology.

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Literature
go back to reference Amrousse R, Katsumi T, Azuma N, Hatai K, Ikeda H, Hori K (2016) Development of green propellants for future space applications. Sci Technol Energ Mater 77:105–110 Amrousse R, Katsumi T, Azuma N, Hatai K, Ikeda H, Hori K (2016) Development of green propellants for future space applications. Sci Technol Energ Mater 77:105–110
go back to reference Anderson FA (1979) High performance ammonium nitrate propellant. US patent 4158583 Anderson FA (1979) High performance ammonium nitrate propellant. US patent 4158583
go back to reference Berg S, Rovey J (2012) Dual-mode propellant properties and performance analysis of energetic ionic liquids. In: 50th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition. American Institute of Aeronautics and Astronautics, Nashville, Tennessee. https://doi.org/10.2514/6.2012-975 Berg S, Rovey J (2012) Dual-mode propellant properties and performance analysis of energetic ionic liquids. In: 50th AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition. American Institute of Aeronautics and Astronautics, Nashville, Tennessee. https://​doi.​org/​10.​2514/​6.​2012-975
go back to reference Calabro M (2011) Overview on hybrid propulsion. EUCASS Proc Ser Adv Aerosp Sci 2:353–374 Calabro M (2011) Overview on hybrid propulsion. EUCASS Proc Ser Adv Aerosp Sci 2:353–374
go back to reference Denisjuk AP, Shepelev YG, Balojan BM, Demidova LA (1996) Low-toxic burning rate catalysts for double base propellants. Energ Mater Technol Manuf Process 71–76 Denisjuk AP, Shepelev YG, Balojan BM, Demidova LA (1996) Low-toxic burning rate catalysts for double base propellants. Energ Mater Technol Manuf Process 71–76
go back to reference Doll D, Lund G (1991) Magnesium-neutralized clean propellant. In: 27th joint propulsion conference. American Institute of Aeronautics and Astronautics Doll D, Lund G (1991) Magnesium-neutralized clean propellant. In: 27th joint propulsion conference. American Institute of Aeronautics and Astronautics
go back to reference Eurospace (2020) Revised space industry position 2020: exemption of propellant-related use of hydrazine and other liquid propellants from the REACH authorisation requirement Eurospace (2020) Revised space industry position 2020: exemption of propellant-related use of hydrazine and other liquid propellants from the REACH authorisation requirement
go back to reference German BJ, Caleb Branscome E, Frits AP, Yiakas NC, Mavris DN (2000) An evaluation of green propellants for an ICBM post-boost propulsion system. Accession number: ADA386589 German BJ, Caleb Branscome E, Frits AP, Yiakas NC, Mavris DN (2000) An evaluation of green propellants for an ICBM post-boost propulsion system. Accession number: ADA386589
go back to reference Gotzig U (2017) Challenges and economic benefits of green propellants for satellite propulsion. In: Conference: 7th European conference for aeronautics and space sciences (EUCASS) Gotzig U (2017) Challenges and economic benefits of green propellants for satellite propulsion. In: Conference: 7th European conference for aeronautics and space sciences (EUCASS)
go back to reference Haeseler D, Bombelli V, Vuillermoz P, Lo R, Marée T, Caramelli F (2004) Green propellant propulsion concepts for space transportation and technology development needs. In: 2nd international conference on green propellants for space propulsion. Cagliari, Sardinia, Italy Haeseler D, Bombelli V, Vuillermoz P, Lo R, Marée T, Caramelli F (2004) Green propellant propulsion concepts for space transportation and technology development needs. In: 2nd international conference on green propellants for space propulsion. Cagliari, Sardinia, Italy
go back to reference Hamilton RS, Wardle RB, Hughes CD, Mancini VE, Dewey MA (1999) A fully recyclable oxetane TPE rocket propellant. Energ Mater Model phenomena. Exp Charact Environ Eng 40–41 Hamilton RS, Wardle RB, Hughes CD, Mancini VE, Dewey MA (1999) A fully recyclable oxetane TPE rocket propellant. Energ Mater Model phenomena. Exp Charact Environ Eng 40–41
go back to reference Heiser WH, Pratt DT (1994) Hypersonic air breathing propulsion. American Institute of Aeronautics and Astronautics, Washington, DC, USA Heiser WH, Pratt DT (1994) Hypersonic air breathing propulsion. American Institute of Aeronautics and Astronautics, Washington, DC, USA
go back to reference Igarashi S, Matsuura Y (2017) Development status of a hydrazine alternative and low- cost thruster using HAN-HN based green propellant. In: 53rd AIAA/SAE/ASEE joint propulsion conference. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-5000 Igarashi S, Matsuura Y (2017) Development status of a hydrazine alternative and low- cost thruster using HAN-HN based green propellant. In: 53rd AIAA/SAE/ASEE joint propulsion conference. American Institute of Aeronautics and Astronautics. https://​doi.​org/​10.​2514/​6.​2017-5000
go back to reference Kappenstein C, Courthéoux L, Eloirdi R, Rossignol S, Duprez D, Pillet N (2002) Catalytic decomposition of HAN-water binary mixtures. In: 38th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit. Institute of Aeronautics and Astronautics (AIAA), Indianapolis, Indiana, USA Kappenstein C, Courthéoux L, Eloirdi R, Rossignol S, Duprez D, Pillet N (2002) Catalytic decomposition of HAN-water binary mixtures. In: 38th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit. Institute of Aeronautics and Astronautics (AIAA), Indianapolis, Indiana, USA
go back to reference Katzakian A, Grix C (2012) High performance electrically controlled solution solid propellant. US patent 8317952 Katzakian A, Grix C (2012) High performance electrically controlled solution solid propellant. US patent 8317952
go back to reference Lyne C, Rovey J, Berg S (2021) Monopropellant-electrospray multimode thruster testing results: electrospray mode. In: AIAA propulsion and energy 2021 forum. American Institute of Aeronautics and Astronautics, AIAA Propulsion and Energy Forum. https://doi.org/10.2514/6.2021-3439 Lyne C, Rovey J, Berg S (2021) Monopropellant-electrospray multimode thruster testing results: electrospray mode. In: AIAA propulsion and energy 2021 forum. American Institute of Aeronautics and Astronautics, AIAA Propulsion and Energy Forum. https://​doi.​org/​10.​2514/​6.​2021-3439
go back to reference McQuaid MJ (2002) Computationally based design and screening of hydrazine-alternative hypergolic fuels. In: Proceeding of the 23th army science conference, Orlando, FL, USA McQuaid MJ (2002) Computationally based design and screening of hydrazine-alternative hypergolic fuels. In: Proceeding of the 23th army science conference, Orlando, FL, USA
go back to reference Oyumi Y, Kimura E, Hayakawa S, Nakashita G, Kato K (1996) Insensitive munitions (IM) and combustion characteristics of GAP/AN composite propellants. Propellants Explos Pyrotech 21:271–275CrossRef Oyumi Y, Kimura E, Hayakawa S, Nakashita G, Kato K (1996) Insensitive munitions (IM) and combustion characteristics of GAP/AN composite propellants. Propellants Explos Pyrotech 21:271–275CrossRef
go back to reference Sayles DC (1975) Propellant composition of the nitrocellulose type containing non lead-containing ballistic modifiers. United States Patent 3860462 Sayles DC (1975) Propellant composition of the nitrocellulose type containing non lead-containing ballistic modifiers. United States Patent 3860462
go back to reference Zhao F-Q, Xu H-X (2011) Research situation and prospect of green solid propellant. Chin J Explos Propellants 34:1–5 Zhao F-Q, Xu H-X (2011) Research situation and prospect of green solid propellant. Chin J Explos Propellants 34:1–5
Metadata
Title
An Overview of Green Propellants and Propulsion System Applications: Merits and Demerits
Authors
Wai Siong Chai
Linlin Liu
Xing Sun
Xinyang Li
Yu-Ying Lu
Copyright Year
2024
DOI
https://doi.org/10.1007/978-3-031-62574-9_1

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