October 2024
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14 Reads
Nuclear Technology
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October 2024
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14 Reads
Nuclear Technology
August 2024
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37 Reads
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1 Citation
Recent trends in research and development on in-space propulsion have advanced the use of the “green propellants” on an ample scale, mainly eyeing environmental sustainability and especially addressing the handling safety concerns. Small satellites, in particular micro and nanosatellites, have advanced from passive orbiting to having the ability to perform active orbital operations with considerable responsiveness, which tends to call for relatively high-thrust impulsive capabilities. Deep space exploration spacecraft of small size with high ΔV requirements, either intended for Lunar exploration or beyond, necessitate the use of storable propellants to support these relatively high-thrust capabilities, as was seen in several CubeSat missions recently (i.e., 2021 onwards) launched to, or intended for, such missions. Hence, onboard propulsion systems sufficing such requirements, while maintaining the now inevitable environmental sustainability standards, are more sought than before. Green propellants for micro propulsion take a major role and a specific attention in small-sized spacecraft design because of their evident potential in replacing conventional propellants. Green propellants demonstrated comparable, or even higher, performance and above all much less safety concerns in handling, storage, and transportability. Safer-to-handle green propellants reduce a significant financial burden for small and medium-sized enterprises, academic institutions, and innovators who are involved in R&D activities in the field of propulsion systems and space systems development.
July 2024
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137 Reads
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1 Citation
Acta Astronautica
This paper presents a comprehensive framework for designing in-space propulsion systems, integrating four criteria: global propulsive performance, environmental impact, cost efficiency, and architectural reliability. The study focuses on the emerging class of Orbital Transfer Vehicles to illustrate the application of this method. By examining the synergistic potential of OTVs and greener propellants, the paper addresses different mission scenarios, including LEO, GEO, and lunar missions, with both scientific and commercial objectives. The proposed framework aims to go beyond traditional cost-centric approaches, offering a more complete evaluation method for early design phases. A case study comparing three liquid bipropellant options, pressure-fed MON-3/MMH, 98%-HTP/RP-1, and self-pressurizing N2O/Ethane, demonstrates the utility of the tool. Findings suggest that scientific missions benefit most from 98%-HTP/RP-1, while traditional propellants remain preferable for cost-driven commercial missions to GEO and the MOON, though greener alternatives are competitive for less demanding LEO missions. This innovative framework aims to guide the selection of propulsion systems to achieve greener space missions, aligning traditional performance figures with environmental responsibility.
May 2024
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29 Reads
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1 Citation
As space activities continue to expand, with increasing numbers of launches and payloads, it becomes crucial to evaluate the environmental consequences of these developments. In this perspective, this study investigates the ground-phase environmental footprint of future in-space liquid bipropellant systems, focusing on MON3/MMH, 98%-HTP/RP-1, 98%-HTP/Ethanol, and N2O/Ethane. A lifecycle analysis from propellant production to the integration of the propulsion system into the launcher for a typical mission scenario identifies key environmental impact hotspots. The findings reveal that the production phase of MMH stands out as particularly detrimental, primarily due to its energy-demanding distillation process and its specialized, low-volume production tailored for space applications. The MON3/MMH system continues to show the highest contribution when considering the entire phases up to propellant loading due to stringent fuelling and decontamination processes. In terms of propulsive architecture, tank production, whether using titanium or aluminium, stands out as the primary environmental hotspot for dry architectures, with titanium proving more environmentally disruptive. In contrast, for wet architectures, the production of dry components constitutes most of the environmental impact, accounting for 95% of the total for HTP combinations and 64% for both MON3/MMH and self-pressurizing options.
March 2024
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102 Reads
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10 Citations
Acta Astronautica
January 2024
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62 Reads
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10 Citations
Astronautica Acta
January 2024
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59 Reads
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1 Citation
January 2024
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26 Reads
January 2024
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5 Reads
January 2024
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18 Reads
... Their ability to maintain structural integrity at high temperatures and high pressures ensures consistent catalytic performance against the deactivation of granular surfaces . The interconnected porosity of cellular ceramics allows for a high surface area-to-volume ratio, promoting optimal interaction between reactants and the catalytic surface, ensuring maximum catalytic efficiency, which is vital for the effective propulsion and maneuvering of spacecraft (Remissa et al., 2023;Souagh et al., 2022;Amrousse et al., 2015;Amrousse et al., 2024;Amrousse et al., 2012;Harimech et al., 2023b;2022;Mansurov et al., 2020;Atamanov et al.;Remissa et al., 2024;Nosseir et al., 2024;Chai et al., 2024;Kumari et al., 2024;Ercan et al., 2024). ...
August 2024
... Values are normalized and presented as percentages relative to the highest impact option, MON-3/MMH, for all scenarios. These values were primarily derived from the single-score total impact, combining results from 15 impact indicators, as detailed in the related publication [29]. Fig. 6. ...
May 2024
... Highly dynamic manoeuvres and long-term satellite missions require chemical propulsion, which brings the storability of propellant to the table. For years, conventional propellants have been mainly based on hydrazine and its derivatives [5][6][7]. The problem is that despite the acceptable performance (specific impulse: N 2 H 4 -220 s [8]), they are highly toxic, inflammable and carcinogenic [9,10], which influences the cost and safety of production, transport and ground handling in general. ...
July 2024
Acta Astronautica
... Furthermore, the presence of condensed species during expansion, as indicated by the asterisk in the data, highlights the need for careful consideration of all factors that may impact the overall efficiency and effectiveness of the bipropellant system. (Sarritzu & Pasini, 2024 Among the various other green alternatives, it is important to highlight water propulsion, which, although is still in its early stages of development, holds significant potential benefits for the sector. Water is easily transportable, can be stored indefinitely, is relatively abundant in space, and is simple to resupply. ...
January 2024
Astronautica Acta
... Hydrogen peroxide can be used as a one-component or two-component propellant. Utilized in a bipropellant system, H 2 O 2 acts as the oxidizer for fuels like hydrazine [7][8][9][10]. When used as a one-component propellant, the easily chemically induced catalytic decomposition reaction of the hydrogen peroxide into gaseous water vapour and oxygen is used to generate thrust [4,11]. ...
March 2024
Acta Astronautica
... Relative cost figures are expressed as percentages of the most expensive one. More detailed computations can be found in the related publication [24]. ...
January 2024
... • A "Greener Hypergolic" option using 98%-HTP with Ethanol or RP-1, adopted in various recent systems [1]. • A "Self-Pressurizing" system combining Nitrous Oxide with Ethane or similar light hydrocarbons with high vapor-pressure [3]. Initially, the paper presents an overview of these systems, setting the stage for a detailed analysis of their environmental footprints from propellant manufacture to system loading for a generic orbital stage mission scenario. ...
January 2024
... Rocket for Agile Cislunar Operations (DRACO) project under an agreement between the Defense Advanced Research Projects Agency (DARPA) and the National Aeronautics and Space Administration (NASA), which is proposed to be an unmanned nuclear thermal rocket that is planned to be demonstrated in 2027 [4]. Given the rapid pace at which this technology must be developed, accurate and reliable NTP simulation and modeling is imperative [5]. This need was emphasized by the National Academy of Science, Engineering, and Medicine in a study [6] that focused on the requirements to mature NTP technology. ...
September 2022
... As the number of payloads and missions increases, there is a growing need for robust in-space logistics systems, comparable to those on Earth, to efficiently handle the influx of new systems and assist them toward potentially longmissions. Central to this discussion is the orbital stage, which operates similarly to Earth's public transportation systems by offering rideshare capabilities that reorganize the logistics of deploying and managing payloads in space [8]. This strategy not only simplifies space operations but also meets the growing demands for on-orbit servicing. ...
January 2023
International Journal of Energetic Materials and Chemical Propulsion
... In the framework of the FLPP programme at the Space Transportation Directorate of ESA, which aims at fostering the implementation of novel technologies, the use of green storable propellants was preferred to more traditional ones. More specifically, the identification of a suitable HTP/Hydrocarbon combination was favoured [14]. ...
June 2022