참고문헌 (41)

1. Aircr. Eng. Okninski 88 480 2016 10.1108/AEAT-07-2014-0106 Rocket rotating detonation engine flight demonstrator 

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2. J. Spacecr. Rockets Kobald 55 484 2017 10.2514/1.A34035 Hybrid experimental rocket stuaettgart: a low-cost technology demonstrator 

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3. Aerosp. Sci. Technol. Marciniak 73 19 2018 10.1016/j.ast.2017.11.034 Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation 

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4. Acta Astronaut. Nowakowski 138 374 2017 10.1016/j.actaastro.2017.06.007 Development of small solid rocket boosters for the ILR-33 sounding rocket 

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5. Acta Astronaut. Nagata 59 253 2006 10.1016/j.actaastro.2006.02.031 Development of CAMUI hybrid rocket to create a market for small rocket experiments 

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6. Acta Astronaut. Okninski 108 46 2015 10.1016/j.actaastro.2014.12.001 Development of the Polish small sounding rocket program 

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7. Apel 3 2016 AQUASONIC-A Sounding Rocket Based on Hybrid Propulsion, Applied Mechanics and Materials 

8. Trans. Jpn. Soc. Aeronaut. Space Sci. Davide Benini 1 2017 Skyward Rocksanne Program: students' sounding rocket as technology demonstrator 

9. J. Spacecr. Rockets Montenbruck 41 644 2004 10.2514/1.1962 Global positioning system sensor with instantaneous-impact-point prediction for sounding rockets 

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10. Pepermans 2017 Comparison of Various Parachute Deployment Systems for Full Rocket Recovery of Sounding Rockets 

11. Poli 439 2016 2016 IEEE Metrology for Aerospace (MetroAeroSpace) Autonomous re-entry system technology demonstrator for sounding rockets: development of an automated control system as recovery device for precise landing of sounding rockets 

12. Int. J. Aeronaut. Space Sci. Huh 18 512 2017 10.5139/IJASS.2017.18.3.512 Development of a university-based simplified H2O2/PE hybrid sounding rocket at KAIST 

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13. Karabeyoglu 2003 Powered Flight - The Next Century Development of high-burning-rate hybrid-rocket-fuel flight demonstrators 

14. J. Propuls. Power Ventura 11 562 1995 10.2514/3.23878 Hydrogen peroxide as an alternate oxidizer for a hybrid rocket booster 

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15. J. Propuls. Power Jung 30 514 2014 10.2514/1.B34739 Autoignitable and restartable hybrid rockets using catalytic decomposition of an oxidizer 

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16. J. Propuls. Power Ahn 34 1189 2018 10.2514/1.B36949 Design of multiport grain with hydrogen peroxide hybrid rocket 

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17. Kang 4864 2016 52nd AIAA/SAE/ASEE Joint Propulsion Conference Design and performance evaluation of hybrid rocket using 95 wt.% H2O2 

18. Yun 4526 2018 2018 Joint Propulsion Conference Demonstration of 2,500 N-class H2O2/HDPE hybrid rocket for lab-scale sounding rocket 

19. Gordon 1994 Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications. Part 1: Analysis 

20. Aerosp. Sci. Technol. Bouziane 89 392 2019 10.1016/j.ast.2019.04.009 Performance comparison of oxidizer injectors in a 1-kN paraffin-fueled hybrid rocket motor 

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21. J. Propuls. Power An 25 1041 2009 10.2514/1.40822 Scaling and evaluation of Pt/Al2O3 catalytic reactor for hydrogen peroxide monopropellant thruster 

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22. J. Propuls. Power An 27 422 2011 10.2514/1.48939 Chugging instability of H2O2 monopropellant thrusters with reactor aspect ratio and pressures 

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23. Aerosp. Sci. Technol. Jo 60 1 2017 10.1016/j.ast.2016.10.022 Response characteristics of H2O2 monopropellant thrusters with MnO2-mixed PbO catalyst 

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24. Aerosp. Sci. Technol. Okninski 82 284 2018 10.1016/j.ast.2018.08.036 Multidisciplinary optimisation of bipropellant rocket engines using H2O2 as oxidiser 

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25. Aerosp. Sci. Technol. Heo 78 26 2018 10.1016/j.ast.2018.03.032 Effect of dual-catalytic bed using two different catalyst sizes for hydrogen peroxide thruster 

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26. J. Aerosp. Technol. Manag. Kafafy 6 69 2014 10.5028/jatm.v6i1.268 Effect of varying design options on the transient behavior of a hybrid rocket motor 

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27. J. Propuls. Power Kim 29 573 2013 10.2514/1.B34619 Regression characteristics of the cylindrical multiport grain in hybrid rockets 

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28. Aerosp. Sci. Technol. Tian 42 334 2015 10.1016/j.ast.2015.01.015 Ignition theory investigation and experimental research on hybrid rocket motor 

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29. Aerosp. Sci. Technol. Lestrade 92 1 2019 10.1016/j.ast.2019.05.057 Experimental demonstration of an end-burning swirling flow hybrid rocket engine 

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30. Int. J. Aerosp. Eng. Huh 2018 2018 10.1155/2018/5630587 Preliminary assessment of hydrogen peroxide gel as an oxidizer in a catalyst ignited hybrid thruster 

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31. Chowdhury 2012 Design and Performance Simulation of a Hybrid Sounding Rocket 

32. J. Aerosp. Technol. Manag. Panta 10 2018 10.5028/jatm.v10.752 Dynamics of a small unmanned aircraft parachute system 

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33. Knacke 1991 Parachute Recovery Systems Design Manual 

34. Aeronaut. Aerosp. Open Access J. Mohammad Samani 1 64 2017 Designing a universal deceleration system for sounding rockets lighter than 100 kg by system engineering approach 

35. J. Spacecr. Rockets Jamison 4 498 1967 10.2514/3.28894 A method for calculating parachute opening forces for general deployment conditions 

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36. J. Spacecr. Rockets Guidotti 49 700 2012 10.2514/1.A32163 Design, development, testing, and in-flight qualification of a parachute recovery system 

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37. Ewing 1979 Recovery System Design Guide 

38. J. Aircr. Peterson 23 87 1986 10.2514/3.45271 Application of Kevlar to parachute system design 

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39. Bisplinghoff 2013 Aeroelasticity 

40. Martin 1951 Summary of Flutter Experiences as a Guide to the Preliminary Design of Lifting Surfaces on Missiles 

41. Barrowman 1966 The theoretical prediction of the center of pressure 

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