Skip to main content
Top

2024 | OriginalPaper | Chapter

8. Hydrogen Peroxide Propulsion: Past Uses and Future Perspectives

Authors : Adrian Parzybut, Pawel Surmacz

Published in: Recent Advancements in Green Propulsion

Publisher: Springer Nature Switzerland

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

In the realm of rocket propulsion, hydrogen peroxide has been a subject of historical intrigue and modern fascination. This comprehensive study delves into the evolution of high-concentration hydrogen peroxide as a propellant, aiming to elucidate its potential in future rocketry and satellite propulsion. Beginning with the pioneers and challenges in The Early Days of Hydrogen Peroxide, it explores innovative European contributions and significant advancements in hydrogen peroxide propulsion in Russia. Subsequently, past endeavours with hydrogen peroxide propulsion in the United States are highlighted. Additionally, the authors dispel misconceptions about hydrogen peroxide. Satellite propulsion emerges as a crucial focus, detailing contemporary applications and exploring future perspectives. Delving into the essential parameters of hydrogen peroxide, the chapter provides a holistic understanding of its characteristics. Present uses showcase its relevance today, while the discussion of temporal postponement sheds light on setbacks faced. The chapter ends by drawing insightful conclusions, emphasizing the promising trajectory of hydrogen peroxide. This comprehensive exploration serves as a valuable resource, guiding future research and shaping the landscape of space propulsion.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
go back to reference Adzhyan AP, Rakhmanin VF (2010) The evolution of progress gas generator of liquid rocket engine. Dvigatel 2:13–15 Adzhyan AP, Rakhmanin VF (2010) The evolution of progress gas generator of liquid rocket engine. Dvigatel 2:13–15
go back to reference Afanas’ev I (2004) Novosti Kosmonavtiki 263:52–55 Afanas’ev I (2004) Novosti Kosmonavtiki 263:52–55
go back to reference An S, Lim H, Kwon S (2007) Hydrogen peroxide thruster module for microsatellites with platinum supported by alumina as catalyst. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://doi.org/10.2514/6.2007-5467 An S, Lim H, Kwon S (2007) Hydrogen peroxide thruster module for microsatellites with platinum supported by alumina as catalyst. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://​doi.​org/​10.​2514/​6.​2007-5467
go back to reference An S, Brahmi R, Kappenstein C, Lee J, Kwon S (2009) Pulse response times of hydrogen peroxide monopropellant thrusters. Paper presented at the 45th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Denver, CO, 2–5 Aug 2009. https://doi.org/10.2514/6.2009-5230 An S, Brahmi R, Kappenstein C, Lee J, Kwon S (2009) Pulse response times of hydrogen peroxide monopropellant thrusters. Paper presented at the 45th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Denver, CO, 2–5 Aug 2009. https://​doi.​org/​10.​2514/​6.​2009-5230
go back to reference Andrews D (1990) Advantages of hydrogen peroxide as a rocket oxidant. J Br Interplanet Soc 43:319–321 Andrews D (1990) Advantages of hydrogen peroxide as a rocket oxidant. J Br Interplanet Soc 43:319–321
go back to reference Baker D (1978) The rocket: the history and development of rocket & missile technology, first edn. Crown Baker D (1978) The rocket: the history and development of rocket & missile technology, first edn. Crown
go back to reference Baker D (2017) NASA mercury manual (owners’ workshop manual). Haynes Publishing Group P.L.C Baker D (2017) NASA mercury manual (owners’ workshop manual). Haynes Publishing Group P.L.C
go back to reference Baltitude J, Burkhardt Z, Harris M, Jalderda M, Suresh SA, Fettes L, Faber D, Schiel J, Cho J, Levitt D (2021) Development and launch of the world’s first orbital propellant tanker. Paper presented at the 35th annual small satellite conference, online conference, 6–11 Aug 2021 Baltitude J, Burkhardt Z, Harris M, Jalderda M, Suresh SA, Fettes L, Faber D, Schiel J, Cho J, Levitt D (2021) Development and launch of the world’s first orbital propellant tanker. Paper presented at the 35th annual small satellite conference, online conference, 6–11 Aug 2021
go back to reference Barley S, Palmer P, Wallbank J, Baker A (2005) Characterisation of a monopropellant microthruster catalytic bed. Paper presented at the 41st AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Tucson, AZ, 10–13 July 2005. https://doi.org/10.2514/6.2005-4544 Barley S, Palmer P, Wallbank J, Baker A (2005) Characterisation of a monopropellant microthruster catalytic bed. Paper presented at the 41st AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Tucson, AZ, 10–13 July 2005. https://​doi.​org/​10.​2514/​6.​2005-4544
go back to reference Becklake J (1990) The British black knight rocket. J Br Interplanet Soc 43:283–290 Becklake J (1990) The British black knight rocket. J Br Interplanet Soc 43:283–290
go back to reference Bell Aerosystems Co (1965) Reaction control system design data for space vehicle applications. Technical rote 8500-95006 Bell Aerosystems Co (1965) Reaction control system design data for space vehicle applications. Technical rote 8500-95006
go back to reference Casu S, Geiger B, Kiemel R, Lestrade JY, Anthoine J (2019) Development and characterization of a catalyst for the decomposition of hydrogen peroxide. Paper presented at the AIAA propulsion and energy 2019 forum, Indianapolis, IN, 19–22 Aug 2019. https://doi.org/10.2514/6.2019-4278 Casu S, Geiger B, Kiemel R, Lestrade JY, Anthoine J (2019) Development and characterization of a catalyst for the decomposition of hydrogen peroxide. Paper presented at the AIAA propulsion and energy 2019 forum, Indianapolis, IN, 19–22 Aug 2019. https://​doi.​org/​10.​2514/​6.​2019-4278
go back to reference Cervone A, Torre L, d’Agostino L, Musker AJ, Roberts GT, Bramanti C, Saccoccia G (2006) Development of hydrogen peroxide monopropellant Rocktes. Paper presented at the 42nd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cologne. https://doi.org/10.2514/6.2006-5239 Cervone A, Torre L, d’Agostino L, Musker AJ, Roberts GT, Bramanti C, Saccoccia G (2006) Development of hydrogen peroxide monopropellant Rocktes. Paper presented at the 42nd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cologne. https://​doi.​org/​10.​2514/​6.​2006-5239
go back to reference Davis DD, Dee LA, Greene B, Hornung SD, McClure MB, Rathgeber KA (2004) Fire, explosion, compatibility and safety hazards of hydrogen peroxide. NASA/TM-2004-213151 Davis DD, Dee LA, Greene B, Hornung SD, McClure MB, Rathgeber KA (2004) Fire, explosion, compatibility and safety hazards of hydrogen peroxide. NASA/TM-2004-213151
go back to reference Faenza MG, Boiron JA, Haemmerli B, Verberne O (2019) The Nammo nucleus launch: Norwegian hybrid sounding rocket over 100 km. Paper presented at the AIAA propulsion and energy 2019 forum, Indianapolis, IN, 19–22 Aug 2019. https://doi.org/10.2514/6.2019-4049 Faenza MG, Boiron JA, Haemmerli B, Verberne O (2019) The Nammo nucleus launch: Norwegian hybrid sounding rocket over 100 km. Paper presented at the AIAA propulsion and energy 2019 forum, Indianapolis, IN, 19–22 Aug 2019. https://​doi.​org/​10.​2514/​6.​2019-4049
go back to reference Ferlin M (2015) Safety evaluation and experience of hydrogen peroxide in launchers domain at guiana space centre. Paper presented at the 7th IAASS conference: space safety is no accident Ferlin M (2015) Safety evaluation and experience of hydrogen peroxide in launchers domain at guiana space centre. Paper presented at the 7th IAASS conference: space safety is no accident
go back to reference Gordon S, McBride, BJ (1996) Computer program for calculation of complex chemical equilibrium compositions and applications—II. Users manual and program description. NASA Reference Publication 1311 Gordon S, McBride, BJ (1996) Computer program for calculation of complex chemical equilibrium compositions and applications—II. Users manual and program description. NASA Reference Publication 1311
go back to reference Gotzig U, Wurdak, M, Lauck F (2018) Development of a flight type 1N hydrogen peroxide thruster. Paper presented at the space propulsion conference, Seville, Spain Gotzig U, Wurdak, M, Lauck F (2018) Development of a flight type 1N hydrogen peroxide thruster. Paper presented at the space propulsion conference, Seville, Spain
go back to reference Hacker BC, Grimwood JM (1977) On the shoulders of titans. A history of project Gemini. Scientific and Technical Information Office, Washington, DC, USA Hacker BC, Grimwood JM (1977) On the shoulders of titans. A history of project Gemini. Scientific and Technical Information Office, Washington, DC, USA
go back to reference Haemmerli B, Digre D, Joraholmen T, Lillekvelland R, Solerod H, Valle T, White J, Mcguiness E, Larkin B, Torre L et al (2021) Overview of the development of a H2O2 based chemical attitude control system for VEGA-C. In: Proceedings of the paper presented at the 7th edition of space propulsion conference 2020+1, Estoril, Portugal Haemmerli B, Digre D, Joraholmen T, Lillekvelland R, Solerod H, Valle T, White J, Mcguiness E, Larkin B, Torre L et al (2021) Overview of the development of a H2O2 based chemical attitude control system for VEGA-C. In: Proceedings of the paper presented at the 7th edition of space propulsion conference 2020+1, Estoril, Portugal
go back to reference Haeseler D (1992) Information from NPO Energomash museum exhibit Haeseler D (1992) Information from NPO Energomash museum exhibit
go back to reference Harlow J (1993) Alpha, beta and RTV-1, the development of early British liquid propellant rocket engines. Paper presented at the 44th congress of the international astronautical federation, Graz, 16–22 Oct 1993 Harlow J (1993) Alpha, beta and RTV-1, the development of early British liquid propellant rocket engines. Paper presented at the 44th congress of the international astronautical federation, Graz, 16–22 Oct 1993
go back to reference Harlow J (1999) Hydrogen peroxide engines—early work on thermal ignition at Westcott. Paper presented at the 2nd international hydrogen peroxide propulsion conference, Purdue University, West. Lafayette, IN Harlow J (1999) Hydrogen peroxide engines—early work on thermal ignition at Westcott. Paper presented at the 2nd international hydrogen peroxide propulsion conference, Purdue University, West. Lafayette, IN
go back to reference Houston RS, Hallion RP, Boston RG (1998) Transiting from air to space: the North American X-15. The hypersonic revolution. In: Case studies in the history of hypersonic technology. Air Force History and Museums Program 1 Houston RS, Hallion RP, Boston RG (1998) Transiting from air to space: the North American X-15. The hypersonic revolution. In: Case studies in the history of hypersonic technology. Air Force History and Museums Program 1
go back to reference Jaffe L (1965) Satellite communications: six years of achievement 1958 through 1964. N66-14276 Jaffe L (1965) Satellite communications: six years of achievement 1958 through 1964. N66-14276
go back to reference Jones CW, Clark JH (1999a) Chapter 1: introduction to the preparation and properties of hydrogen peroxide. In: Applications of hydrogen peroxide and derivatives, pp 1–36 Jones CW, Clark JH (1999a) Chapter 1: introduction to the preparation and properties of hydrogen peroxide. In: Applications of hydrogen peroxide and derivatives, pp 1–36
go back to reference Koopmans R-J, Nandyala V, Pavesi S, Ceribas E, Batonneau Y, Maleix C, Beauchet R, Schwentenwein M, Spitzbart M, Altun A, Mione M, Scharlemann C (2018) Influence of catalyst geometry on performance of catalysts for green propellant thrusters. Paper presented at the space propulsion conference, Seville, Spain Koopmans R-J, Nandyala V, Pavesi S, Ceribas E, Batonneau Y, Maleix C, Beauchet R, Schwentenwein M, Spitzbart M, Altun A, Mione M, Scharlemann C (2018) Influence of catalyst geometry on performance of catalysts for green propellant thrusters. Paper presented at the space propulsion conference, Seville, Spain
go back to reference Krejci D, Woschnak A, Schiebl M, Scharlemann C, Ponweiser K, Brahmi R, Batonneau Y, Kappenstein C (2013) Assessment of catalysts for hydrogen-peroxide-based thrusters in a flow reactor. J Propul Power 29(2). https://doi.org/10.2514/1.B34615 Krejci D, Woschnak A, Schiebl M, Scharlemann C, Ponweiser K, Brahmi R, Batonneau Y, Kappenstein C (2013) Assessment of catalysts for hydrogen-peroxide-based thrusters in a flow reactor. J Propul Power 29(2). https://​doi.​org/​10.​2514/​1.​B34615
go back to reference Lauck F, Negri M, Wilhelm M et al (2018) Test bench preparation and hot firing tests of a 1N hydrogen peroxide monopropellant thruster. Paper presented at the space propulsion conference, Seville, 14–18 May 2018 Lauck F, Negri M, Wilhelm M et al (2018) Test bench preparation and hot firing tests of a 1N hydrogen peroxide monopropellant thruster. Paper presented at the space propulsion conference, Seville, 14–18 May 2018
go back to reference Lauck F, Balkenhohl J, Negri M, Freudenmann D, Schlechtriem S (2021) Ignition investigations of a novel hypergolic ionic liquid with hydrogen peroxide in drop tests. Paper presented at the space propulsion conference, online conference, 17–19 Mar 2021 Lauck F, Balkenhohl J, Negri M, Freudenmann D, Schlechtriem S (2021) Ignition investigations of a novel hypergolic ionic liquid with hydrogen peroxide in drop tests. Paper presented at the space propulsion conference, online conference, 17–19 Mar 2021
go back to reference Long M, Rusek J (2000) The characterization of the propulsive decomposition of hydrogen peroxide. Paper presented at the 36th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Las Vegas, NV, 24–28 July 2000. https://doi.org/10.2514/6.2000-3683 Long M, Rusek J (2000) The characterization of the propulsive decomposition of hydrogen peroxide. Paper presented at the 36th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Las Vegas, NV, 24–28 July 2000. https://​doi.​org/​10.​2514/​6.​2000-3683
go back to reference Love JE, Stillwell WH (1963) The hydrogen-peroxide rocket reaction-control system for the X-1B research plane. NASA technical note D-185 Love JE, Stillwell WH (1963) The hydrogen-peroxide rocket reaction-control system for the X-1B research plane. NASA technical note D-185
go back to reference Marciniak B, Okninski A, Bartkowiak B, Pakosz M, Sobczak K, Florczuk W, Kaniewski D, Matyszewski J, Nowakowski P, Cieslinski D, Rarata G, Surmacz P, Kublik D, Rysak D, Smetek J, Wolanski P (2018) Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation. Aerosp Sci Technology 73:19–31. https://doi.org/10.1016/j.ast.2017.11.034CrossRef Marciniak B, Okninski A, Bartkowiak B, Pakosz M, Sobczak K, Florczuk W, Kaniewski D, Matyszewski J, Nowakowski P, Cieslinski D, Rarata G, Surmacz P, Kublik D, Rysak D, Smetek J, Wolanski P (2018) Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation. Aerosp Sci Technology 73:19–31. https://​doi.​org/​10.​1016/​j.​ast.​2017.​11.​034CrossRef
go back to reference McCormick J (1965a) Hydrogen peroxide rocket manual. FMC Corporation, Pasadena, TX McCormick J (1965a) Hydrogen peroxide rocket manual. FMC Corporation, Pasadena, TX
go back to reference McCormick J (1965b) Method of decomposing hydrogen peroxide using a silver-palladium catalyst. US Patent 3,488,962, 13 Jan 1970 McCormick J (1965b) Method of decomposing hydrogen peroxide using a silver-palladium catalyst. US Patent 3,488,962, 13 Jan 1970
go back to reference McCormick JC et al (1961) Storage of 90% and 98% by weight hydrogen peroxide in sealed containers for extended periods. AD268379, New York, NY, USA McCormick JC et al (1961) Storage of 90% and 98% by weight hydrogen peroxide in sealed containers for extended periods. AD268379, New York, NY, USA
go back to reference Millward D (2001) The black arrow rocket—a history of a satellite launch vehicle and its engines. Paper presented at the 1st edition. NMSI Trading Ltd., Science Museum, London, UK Millward D (2001) The black arrow rocket—a history of a satellite launch vehicle and its engines. Paper presented at the 1st edition. NMSI Trading Ltd., Science Museum, London, UK
go back to reference Müller K (1937) Industrial applications of high-concentration hydrogen peroxide. J Ind Chem 12:301–305 Müller K (1937) Industrial applications of high-concentration hydrogen peroxide. J Ind Chem 12:301–305
go back to reference Munday TCF, Darbee LR, McCormick JC (1967) Investigation of decomposition catalyst for 98% hydrogen peroxide. Technical report AFRPL-TR-67-80 Munday TCF, Darbee LR, McCormick JC (1967) Investigation of decomposition catalyst for 98% hydrogen peroxide. Technical report AFRPL-TR-67-80
go back to reference Musker AJ, Roberts GT, Rusek JJ, Kappenstein C (2006) Hydrogen peroxide—from bridesmaid to bride. Paper presented at the 3rd international conference on green propellants, poitiers, 17–20 Sept 2006 Musker AJ, Roberts GT, Rusek JJ, Kappenstein C (2006) Hydrogen peroxide—from bridesmaid to bride. Paper presented at the 3rd international conference on green propellants, poitiers, 17–20 Sept 2006
go back to reference Neufeld MJ (1995) The rocket and the Reich: Peenemünde and the coming of the ballistic missile era. New York, NY Neufeld MJ (1995) The rocket and the Reich: Peenemünde and the coming of the ballistic missile era. New York, NY
go back to reference Palmer MJ (2014) Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters. Dissertation, University of Southampton Palmer MJ (2014) Experimental evaluation of hydrogen peroxide catalysts for monopropellant attitude control thrusters. Dissertation, University of Southampton
go back to reference Palmer MJ, Musker AJ, Roberts GT (2011) Experimental assessment of heterogeneous catalysts for the decomposition of hydrogen peroxide. Paper presented at the 47th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, San Diego, CA, 31 July–3 Aug 2011. https://doi.org/10.2514/6.2011-5695 Palmer MJ, Musker AJ, Roberts GT (2011) Experimental assessment of heterogeneous catalysts for the decomposition of hydrogen peroxide. Paper presented at the 47th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, San Diego, CA, 31 July–3 Aug 2011. https://​doi.​org/​10.​2514/​6.​2011-5695
go back to reference Parzybut A, Surmacz P, Gut Z (2022) Development of 1N “green” monopropellant thruster. Testing of most promising catalyst beds for 98% hydrogen peroxide. Paper presented at the space propulsion conference, Estoril, Portugal Parzybut A, Surmacz P, Gut Z (2022) Development of 1N “green” monopropellant thruster. Testing of most promising catalyst beds for 98% hydrogen peroxide. Paper presented at the space propulsion conference, Estoril, Portugal
go back to reference Pasini A, Pace G, Valentini D (2018) Experimental campaign on a 98% H2O2 pulsed thruster. Paper presented at the space propulsion conference, Seville, Spain Pasini A, Pace G, Valentini D (2018) Experimental campaign on a 98% H2O2 pulsed thruster. Paper presented at the space propulsion conference, Seville, Spain
go back to reference Powell JW, Richards GR (1987) The orbiting vehicle series of satellites. J Br Interplanet Soc 40:417–426 Powell JW, Richards GR (1987) The orbiting vehicle series of satellites. J Br Interplanet Soc 40:417–426
go back to reference Przybilski OH (2002) The Germans and the development of rocket engines in the USSR. J Br Interplanet Soc 55:404–427 Przybilski OH (2002) The Germans and the development of rocket engines in the USSR. J Br Interplanet Soc 55:404–427
go back to reference Qingguo L, Xin Q, Yuanding W, Bo Q (2018) Research and development of green propellant engines for space propulsion systems. Paper presented at the space propulsion conference, Seville, Spain Qingguo L, Xin Q, Yuanding W, Bo Q (2018) Research and development of green propellant engines for space propulsion systems. Paper presented at the space propulsion conference, Seville, Spain
go back to reference Rarata G, Surmacz P (2011) The safe preparation of HTP and concentrated H2O2 samples. Trans Inst Aviat 217:116–124 Rarata G, Surmacz P (2011) The safe preparation of HTP and concentrated H2O2 samples. Trans Inst Aviat 217:116–124
go back to reference Romeo L, Torre L, Pasini A, Cervone A, d’Agostino L, Calderazzo F (2007) Performance of different catalysts supported on alumina spheres for hydrogen peroxide decomposition. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://doi.org/10.2514/6.2007-5466 Romeo L, Torre L, Pasini A, Cervone A, d’Agostino L, Calderazzo F (2007) Performance of different catalysts supported on alumina spheres for hydrogen peroxide decomposition. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://​doi.​org/​10.​2514/​6.​2007-5466
go back to reference Runckel JF, Willis CM, Salters LB (1963) Investigation of catalyst beds for 98-percent concentration hydrogen peroxide. NASA Technical Note D-1808 Runckel JF, Willis CM, Salters LB (1963) Investigation of catalyst beds for 98-percent concentration hydrogen peroxide. NASA Technical Note D-1808
go back to reference Schmidt E (1987) One hundred years of hydrazine chemistry. Paper presented at the 3rd conference on environmental chemistry of hydrazine fuels, Panama City Beach, FL Schmidt E (1987) One hundred years of hydrazine chemistry. Paper presented at the 3rd conference on environmental chemistry of hydrazine fuels, Panama City Beach, FL
go back to reference Schreib RR, Pugmire TK, Chapin S (1969) The hybrid (hydrazine) resistojet. Paper presented at the 5th propulsion joint specialist, Colorado Springs, CO, 9–13 June 1969 Schreib RR, Pugmire TK, Chapin S (1969) The hybrid (hydrazine) resistojet. Paper presented at the 5th propulsion joint specialist, Colorado Springs, CO, 9–13 June 1969
go back to reference Schuh S, Bartok T, Koopmans R-J, Scharlemann C (2015) Experimental assessment of hydrogen peroxide compatibility. Paper presented at the 51st AIAA/SAE/ASEE joint propulsion conference, propulsion and energy forum, Orlando, FL, 27–29 July 2015. https://doi.org/10.2514/6.2015-4252 Schuh S, Bartok T, Koopmans R-J, Scharlemann C (2015) Experimental assessment of hydrogen peroxide compatibility. Paper presented at the 51st AIAA/SAE/ASEE joint propulsion conference, propulsion and energy forum, Orlando, FL, 27–29 July 2015. https://​doi.​org/​10.​2514/​6.​2015-4252
go back to reference Schumb WC, Satterfield CN, Weutworth RL (1955) Hydrogen peroxide. A.C.S. Monograph 128, Reinhold Publishing Corporation, New York, NY Schumb WC, Satterfield CN, Weutworth RL (1955) Hydrogen peroxide. A.C.S. Monograph 128, Reinhold Publishing Corporation, New York, NY
go back to reference Sellers JJ, Meerman M, Paul M, Sweeting M (1995) A low-cost propulsion option for small satellites. J Br Interplanet Soc 48:129–138 Sellers JJ, Meerman M, Paul M, Sweeting M (1995) A low-cost propulsion option for small satellites. J Br Interplanet Soc 48:129–138
go back to reference Smith A, Johnson B (1875) Advances in chemical research 3. Academic Press Smith A, Johnson B (1875) Advances in chemical research 3. Academic Press
go back to reference Stokes PR (1998) Hydrogen peroxide for power and propulsion. Paper presented at the science museum, London, UK Stokes PR (1998) Hydrogen peroxide for power and propulsion. Paper presented at the science museum, London, UK
go back to reference Sutton GP, Biblarz O (2000) Rocket propulsion elements, 7th edn. Wiley, New York Sutton GP, Biblarz O (2000) Rocket propulsion elements, 7th edn. Wiley, New York
go back to reference Sviatov G (2003) The Kursk’s loss offers lessons. In: U.S. Naval institute proceedings 129/6/1,204 Sviatov G (2003) The Kursk’s loss offers lessons. In: U.S. Naval institute proceedings 129/6/1,204
go back to reference Syncom Engineering Report, Volume I (1966) NASA TR R-233 Syncom Engineering Report, Volume I (1966) NASA TR R-233
go back to reference Thénard LJ (1818) Discovery and production of hydrogen peroxide. J Paris Acad Sci 5:45–48 Thénard LJ (1818) Discovery and production of hydrogen peroxide. J Paris Acad Sci 5:45–48
go back to reference Ventura M, Garboden G (1999) A brief history of concentrated hydrogen peroxide uses. Paper presented at the 35th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Los Angeles, CA, 20–24 June 1999 Ventura M, Garboden G (1999) A brief history of concentrated hydrogen peroxide uses. Paper presented at the 35th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Los Angeles, CA, 20–24 June 1999
go back to reference Ventura MC, Wernimont EJ (2001) History of the reaction motors super performance 90 percent H2O2/kerosene LR-40 rocket engine. Paper presented at the 37th joint propulsion conference and exhibit, Salt Lake, UT, 8–11 July 2001. https://doi.org/10.2514/6.2001-3838 Ventura MC, Wernimont EJ (2001) History of the reaction motors super performance 90 percent H2O2/kerosene LR-40 rocket engine. Paper presented at the 37th joint propulsion conference and exhibit, Salt Lake, UT, 8–11 July 2001. https://​doi.​org/​10.​2514/​6.​2001-3838
go back to reference Ventura M, Wernimont E, Dillard J (2007a) Hydrogen peroxide—optimal for turbomachinery and power applications. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://doi.org/10.2514/6.2007-5537 Ventura M, Wernimont E, Dillard J (2007a) Hydrogen peroxide—optimal for turbomachinery and power applications. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://​doi.​org/​10.​2514/​6.​2007-5537
go back to reference Ventura M, Wernimont E, Heister S, Yuan S (2007b) Rocket grade hydrogen peroxide (RGHP) for use in propulsion and power devices—historical discussion of hazards. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://doi.org/10.2514/6.2007-5468 Ventura M, Wernimont E, Heister S, Yuan S (2007b) Rocket grade hydrogen peroxide (RGHP) for use in propulsion and power devices—historical discussion of hazards. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://​doi.​org/​10.​2514/​6.​2007-5468
go back to reference Volkov EB (1996) Mezhkontinental’nye Ballisticheskie Rakety SSSR (RF) i SShA (Intercontinental Ballistic Missiles of the Soviet Union (Russian Federation) and United States). RVSN, Moscow Volkov EB (1996) Mezhkontinental’nye Ballisticheskie Rakety SSSR (RF) i SShA (Intercontinental Ballistic Missiles of the Soviet Union (Russian Federation) and United States). RVSN, Moscow
go back to reference Syncom Engineering Report, Volume II (1967) NASA-TR-R-252 Syncom Engineering Report, Volume II (1967) NASA-TR-R-252
go back to reference Walter H (1957) Hydrogen peroxide rockets. In: History of German guided missile developments. AGARDograph 20 Walter H (1957) Hydrogen peroxide rockets. In: History of German guided missile developments. AGARDograph 20
go back to reference Wernimont EJ (2006b) System trade parameter comparison of monopropellants: hydrogen peroxide vs hydrazine and others. Paper presented at the 42nd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Sacramento, CA, 9–12 July 2006. https://doi.org/10.2514/6.2006-5236 Wernimont EJ (2006b) System trade parameter comparison of monopropellants: hydrogen peroxide vs hydrazine and others. Paper presented at the 42nd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Sacramento, CA, 9–12 July 2006. https://​doi.​org/​10.​2514/​6.​2006-5236
go back to reference Wernimont EJ, Durant D (2004) State of the art high performance hydrogen peroxide catalyst beds. Paper presented at the 40th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Lauderdale, FL, 11–14 July 2004. https://doi.org/10.2514/6.2004-4147 Wernimont EJ, Durant D (2004) State of the art high performance hydrogen peroxide catalyst beds. Paper presented at the 40th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Lauderdale, FL, 11–14 July 2004. https://​doi.​org/​10.​2514/​6.​2004-4147
go back to reference Wernimont EJ, Ventura MC (2007) Review of US historical rocket propellants: accidents, mishaps & fatalities. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://doi.org/10.2514/6.2007-5648 Wernimont EJ, Ventura MC (2007) Review of US historical rocket propellants: accidents, mishaps & fatalities. Paper presented at the 43rd AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Cincinnati, OH, 8–11 July 2007. https://​doi.​org/​10.​2514/​6.​2007-5648
go back to reference Wernimont E, Ventura M, Garboden G, Mullens P (1999) Past and present uses of rocket grade hydrogen peroxide. Paper presented at the 2nd international hydrogen peroxide propulsion conference, Hannover, 7–10 Nov 1999 Wernimont E, Ventura M, Garboden G, Mullens P (1999) Past and present uses of rocket grade hydrogen peroxide. Paper presented at the 2nd international hydrogen peroxide propulsion conference, Hannover, 7–10 Nov 1999
go back to reference Werrell KP (1985) The evolution of the cruise missile. Air University Press, Montgomery, ALCrossRef Werrell KP (1985) The evolution of the cruise missile. Air University Press, Montgomery, ALCrossRef
go back to reference Whitehead J (1998) Hydrogen peroxide propulsion for smaller satellites. Paper presented at the 1st international hydrogen peroxide propulsion conference, University of Surrey, UK Whitehead J (1998) Hydrogen peroxide propulsion for smaller satellites. Paper presented at the 1st international hydrogen peroxide propulsion conference, University of Surrey, UK
go back to reference Willis CM (1960) The effect of catalyst-bed arrangement on thrust buildup and decay time for a 90 percent hydrogen peroxide control rocket. National Aeronautics and Space Administration. NASA TN D-516 Willis CM (1960) The effect of catalyst-bed arrangement on thrust buildup and decay time for a 90 percent hydrogen peroxide control rocket. National Aeronautics and Space Administration. NASA TN D-516
go back to reference Wolf S (1963) Hydrogen peroxide as a torpedo propellant. U.S. Naval Underwater Ordnance Station Report 360 Wolf S (1963) Hydrogen peroxide as a torpedo propellant. U.S. Naval Underwater Ordnance Station Report 360
go back to reference Wolf M, Christ P, Goek S, Leininger S (2018) Development of near-anhydrous hydrogen peroxide (≥ 97%) for satellite propulsion and assessment of material compatibility for fluidic components and light weight propellant tanks. Paper presented at the space propulsion conference, Seville, Spain Wolf M, Christ P, Goek S, Leininger S (2018) Development of near-anhydrous hydrogen peroxide (≥ 97%) for satellite propulsion and assessment of material compatibility for fluidic components and light weight propellant tanks. Paper presented at the space propulsion conference, Seville, Spain
go back to reference Wucherer EJ, Cook T, Stiefel M (2003) Hydrazine catalyst production—sustaining S-405 technology. Aerojet, NASA, 2003, Redmond, WA Wucherer EJ, Cook T, Stiefel M (2003) Hydrazine catalyst production—sustaining S-405 technology. Aerojet, NASA, 2003, Redmond, WA
go back to reference Wynn J, Westcott R, Musker AJ (2014) Development of a 10N TRL5 monopropellant thruster using hydrogen peroxide. Paper presented at the space propulsion conference, Cologne, 19–22 May 2014 Wynn J, Westcott R, Musker AJ (2014) Development of a 10N TRL5 monopropellant thruster using hydrogen peroxide. Paper presented at the space propulsion conference, Cologne, 19–22 May 2014
go back to reference Zaloga S (2008) German V-weapon sites 1943–45. Osprey Publishing, Oxford Zaloga S (2008) German V-weapon sites 1943–45. Osprey Publishing, Oxford
Metadata
Title
Hydrogen Peroxide Propulsion: Past Uses and Future Perspectives
Authors
Adrian Parzybut
Pawel Surmacz
Copyright Year
2024
DOI
https://doi.org/10.1007/978-3-031-62574-9_8

Premium Partner