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国际能源材料和化学驱动期刊

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ISSN 打印: 2150-766X

ISSN 在线: 2150-7678

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.7 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 0.7 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.1 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00016 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.18 SJR: 0.313 SNIP: 0.6 CiteScore™:: 1.6 H-Index: 16

Indexed in

HYBRID PROPULSION FOR SMALL SATELLITES DESIGN LOGIC AND TESTS

卷 5, 册 1-6, 2002, pp. 90-100
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.130
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摘要

The objective of the study is to offer an alternative to the propulsion by hydrazine for the positioning and control of micro-satellites or small interplanetary probes, which require high velocity impulse. This paper presents the study of a design and an operation code for polyethylene/H2O2 (87%) hybrid rocket motors. The assumptions used at the moment do not allow for a perfect optimization. The developments which will follow will keep the same logic but with less restrictive hypotheses and more realistic calculations. At the same time, an experimental study has been started with the aim of better understanding the operating range of hybrid rocket motors and the influence of the polyethylene pyrolysis rate in the design. Hybrid rocket motor design and operation have been computed according to the available volume on a micro-satellite.

对本文的引用
  1. Casalino Lorenzo, Letizia Francesca, Pastrone Dario, Design Trade-offs for Hybrid Rocket Motors, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2012. Crossref

  2. Casalino Lorenzo, Letizia Francesca, Pastrone Dario, Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure, Journal of Propulsion and Power, 30, 5, 2014. Crossref

  3. Casalino Lorenzo, Pastrone Dario, Optimization of a Hybrid Rocket Upper Stage with Electric Pump Feed System, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010. Crossref

  4. Casalino Lorenzo, Pastrone Dario, A Straightfotward Approach for Robust Design of Hybrid Rocket Engine Upper Stage, 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015. Crossref

  5. Ingenito Antonella, Bruno Claudio, Using Aluminum for Space Propulsion, Journal of Propulsion and Power, 20, 6, 2004. Crossref

  6. Casalino Lorenzo, Pastrone Dario, Optimization of Hybrid Propellant Mars Ascent Vehicle, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014. Crossref

  7. Casalino Lorenzo, Pastrone Dario, Oxidizer Control and Optimal Design of Hybrid Rocket for Small Satellites, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2003. Crossref

  8. Casalino Lorenzo, Pastrone Dario, Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages, Journal of Propulsion and Power, 26, 3, 2010. Crossref

  9. Casalino Lorenzo, Pastrone Dario, Optimization of Hybrid Sounding Rockets for Hypersonic Testing, Journal of Propulsion and Power, 28, 2, 2012. Crossref

  10. Casalino Lorenzo, Pastrone Dario, Optimal Design of Hybrid Rocket Motors for Microgravity Platform, Journal of Propulsion and Power, 24, 3, 2008. Crossref

  11. Casalino Lorenzo, Masseni Filippo, Pastrone Dario, Optimization of Hybrid Rocket Engines for Small Satellite Launchers, 2018 Joint Propulsion Conference, 2018. Crossref

  12. Benzenine Fadela, Seladji Chakib, Darfilal Djamal, CFD Analysis of Two Supersonic Nozzles Designed for a High Test Peroxide Thruster, 2019 9th International Conference on Recent Advances in Space Technologies (RAST), 2019. Crossref

  13. Dyrda David M., Mechentel Flora S., Cantwell Brian J., Karp Ashley C., Rabinovitch Jason, Jens Elizabeth T., Diode Laser Ignition of a Poly(Methyl Methacrylate) and Gaseous Oxygen Hybrid Motor, Journal of Propulsion and Power, 36, 5, 2020. Crossref

  14. Casalino Lorenzo, Masseni Filippo, Pastrone Dario, Hybrid Rocket Engine Design Optimization at Politecnico di Torino: A Review, Aerospace, 8, 8, 2021. Crossref

  15. Casalino Lorenzo, Masseni Filippo, Pastrone Dario, Optimal Design of Electrically Fed Hybrid Mars Ascent Vehicle, Aerospace, 8, 7, 2021. Crossref

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