[3] M. Ventura e G. Garboden, A brief history of concentrated hydrogen peroxide uses, AIAA Paper 99-2739, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

(1)

[1] W. Anderson, D. Crockett, S. Hill, T. Lewis, R. Fuller, P. Morlan, D. Ruttle, P. K. Wu e C.

McNeal, Low cost propulsion using a high-density, storable and clean propellant combination, AIAA Paper 98-3679

[2] K. Anﬂo, T. A. Gr¨onland, G. Bergman, M. Johansson e R. Nedar, Towards green propulsion for spacecraft with ADN-based monopropellants, AIAA Paper 2002-3847

[3] M. Ventura e G. Garboden, A brief history of concentrated hydrogen peroxide uses, AIAA Paper 99-2739, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

[4] M. Ventura e P. Mullens, The use of hydrogen peroxide for propulsion and power, AIAA Paper 99-2880, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

[5] V. Bombelli, D. Simon, T. Mar´ee e J. L. Moerel, Economic beneﬁts of the use of non-toxic monopropellants for spacecraft applications, AIAA Paper 2003-47, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2003.

[6] P. K. Wu, R. P. Fuller, P. W. Morlan, D. W. Ruttle e A. S. Nejad, Development of a pressure-fed rocket engine using hydrogen peroxide and JP-8, AIAA Paper 99-2877, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

[7] E. J. Wucherer, S. Christoﬀerson e B. Reed, Assessment of high performance HAN monopropellants, AIAA Paper 2000-3872

[8] D. Andrews, Advantages of hydrogen peroxide as a rocket oxidant, Journal of the British interplanetary society, Vol. 43, pp. 319-328, 1990

[9] J. J. Sellers, M. Meerman, M. Paul e M. Sweeting, A low-cost propulsion option for small satellites, Journal of the British interplanetary society, Vol. 48, pp. 129-138, 1995

[10] D. Haeseler, A. G¨otz e A. Fr¨ohlich, Non-toxic propellants for future advanced launch- er propulsion systems, AIAA Paper 2000-3687, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2000

[11] D. L. Hitt, C. M. Zakrzwski e M. A. Thomas, MEMS-based satellite micropropulsion via

catalyzed hydrogen peroxide decomposition, Institute of physics publishing, Vol. 10, pp.1163-

1175, 2001

(2)

[12] A. S. Prince, R. L. Carpenter, T. A. Boardman, T. M. Abel e S. E. Claﬂin, Design and testing of an upper stage hybrid propulsion system using hydrogen peroxide oxidizer, AIAA Paper 2000-3542, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2000

[13] P. Markopoulos e T. Abel, Development and testing of a hydrogen peroxide hybrid up- per stage propulsion system, AIAA Paper 2001-3243, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, USA, July 2001

[14] B. Palaszewski, L. S. Ianovski e P. Carrick, Propellant technologies: a persuasive wave of future propulsion beneﬁts, NASA-TM 97-206228, December 1997

[15] A. Davenas, Chemical propulsion and propellants for space

[16] M. F. Easton, A. G. Mitchell e W. F. K. Wynne-Jones, Trans. Faraday Soc., 48:796, 1952 [17] G. P. Sutton, Rocket propulsion elements - An introduction to the engineering of rockets,

John Wiley and Sons Inc., 1992

[18] G. Scatchard, G. M. Kavanagh e L. B. Ticknor, J. Amer. Chem. Soc., 74:3715-3720, 1952 [19] CEFIC, Hydrogen Peroxide Bulk Storage Guideline

[20] N. Nimmerfroh, E.Walzer, Propulse

^{(T M)}

hydrogen peroxide: manufacture, quality, safety, transportation and handling

[21] N. Nimmerfroh, D. Pauls e S. McMahon, Propulse

^{(T M)}

hydrogen peroxide: manufacture, quality, transportation and handling, AIAA Paper 00-3682, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2000

[22] M. Kroutil e M. Vender, Chem. Prumysl., 14:412-415, 1956 [23] Solvay-Interox, Hydrogen Peroxide - Data Manual, p. 16

[24] Solvay, Scheda di sicurezza - H2O2 HTP 90 Interox High Test Peroxide, 26/04/2004 [25] Solvay, Perossido di Idrogeno, Stoccaggio e Manipolazione, 1999

[26] Solvay, Perossido di Idrogeno, Stoccaggio e Manipolazione- Documentazione tecnica, 2003 [27] Degussa, PROPULSE

^{(T M)}

875 HTP safety data sheet, Degussa document n. 91/155/EWG [28] M. K. Phibbs e P. A. Giguere, Can. J. Chem., 29:173, 1951

[29] C. N. Satterﬁeld, R. L. Wentworth e S. T. Demetriades, J. Amer. Chem. Soc., 76:2623-2637, 1954

[30] J. J. Van Laar, Z. Physik. Chem., 72:723, 1910

[31] P. A. Giguere, Complements au Nouveau Traite de Chimie Minerale - No. 4 - Peroxyde d’Hydrogene et Ployoxydes d’Hydrogene Paris, Masson, 1975, p. 181

[32] R. A. Svehla, NASA Tech. Rpt. R-132, Springﬁeld, 1962, p. 120

(3)

[33] P. A. Giguere, I. D. Liu, J. S. Dugdale e J. A. Morrison, Can. J. Chem., 32:117-128, 1954 [34] P. A. Giguere, I. D. Liu, J. S. Dugdale e J. A. Morrison, Can. J. Chem., 74:3715, 1952 [35] W. C. Schumb, C. N. Satterﬁeld e R. L. Wentworth, Hydrogen Peroxide, ACS Monograph,

Reinhold Publishing Corp., New York, 1955, p. 757

[36] P. M. Gross and R. C. Taylor, J. Amer. Chem. Soc., 72:2075, 1950

[37] M. Ventura e E. Wernimont, Review of hydrogen peroxide material safety data sheets, AIAA Paper 2002-3850, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, July 2002.

[38] M. Ventura e S. Yuan, Commercial production and use of hydrogen peroxide, AIAA Pa- per 2000-3556, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2000

[39] E. Wernimont e P. Mullens, Capabilities of hydrogen peroxide catalist beds, AIAA Paper 00- 3555, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2000

[40] M. R. Long e J. Rusek, The characterization of the propulsive decomposition of hydrogen per- oxide, AIAA Paper 2000-3683, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2000

[41] T. Ali e W. E. Anderson, Hydrogen peroxide stability margin, AIAA Paper 2003-4620, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2003

[42] A. J. Musker, Highly stabilised hydrogen peroxide as a rocket propellant, AIAA Paper 2003- 4619, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 2003

[43] E. Wernimont e M. Ventura, Review of hydrogen peroxide speciﬁcation MIL-P-16005, AIAA Paper 01-3251, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, USA, July 2001

[44] E. Wernimont e P. Mullens, Recent developments in hydrogen peroxide monopropellant de- vices, AIAA Paper 99-2741, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

[45] M. Ventura e E. Wernimont, Advancements in high concentration hydrogen peroxyde catalyst beds, AIAA Paper 01-3250, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, USA, July 2001

[46] L. Pirault-Roy, C. Kappenstein, M. Guerin, R. Eloirdi e N.Pillet, Hydrogen peroxide decom- position on various supported catalysts eﬀect of stabilizers, J. of Propulsion and Power, Vol.

18, no.6, pp. 1235-1241, 2002

[47] P. Morlan, P. Wu, A. Nejad, D. Ruttle, R. Fuller e W. Anderson, Catalyst development

for hydrogen peroxide rocket engines, AIAA Paper 99-2740, 35th AIAA/ASME/SAE/ASEE

Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

(4)

[48] E. J. Wernimont e S. D. Heister, Experimental Study of chamber pressure eﬀects in a hydro- gen peroxide-oxidized hybrid rocket, AIAA Paper 97-2801, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, USA, July 1997

[49] T. R. Beutien, S. D. Heister, J. J. Rusek e S. Meyer, Cordierite-based catalytic beds for 98% hydrogen peroxide, AIAA Paper 2002-3853, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, July 2002

[50] H. Tian, T. Zhang, X. Sun, D. Liang e L. Lin, Performance and deactivation of Ir/γ −Al

₂

O

₃

catalyst in the hydrogen peroxide monopropellant thrusters, Applied Catalysis A:General, 210, 55-62

[51] T. L. Pourpoint e J. J. Rusek, Investigation of homogeneous and heterogeneous catalysis for the propulsive decomposition of hydrogen peroxide

[52] J. S. Mok, J. C. Sisco e W. E. Anderson, Analysis and experiments of hydrogen peroxide vaporization and decomposition, AIAA Paper 2003-4621, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2003

[53] J. H. Corpening, S. D. Heister e W. E. Anderson, A model for thermal decomposition of hy- drogen peroxide, AIAA Paper 2004-3373, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale, USA, July 2004

[54] I. Coxhill, G.Richardson e M. Sweeting, An investigation of a low cost HTP / Kerosene 40 N thruster for small satellites, AIAA Paper 2002-4155, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, July 2002

[55] D. J. Moser, High-performance, non-toxic spacecraft propulsion system development, AIAA Paper 2001-3248, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, USA, July 2001

[56] W. Anderson, C. Johnson e R. Ross, Catalyst bed instability within the USFE H

₂

O

₂

/JP- 8 rocket engine, AIAA Paper 2000-3301, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, USA, June 2000

[57] J. P. Wanhainen, P. S. Ross e R. L. Dewitt, Eﬀects of propellant and catalyst bed temperatures on thrust buildup in several hydrogen peroxide reaction control rockets, NASA Technical Note D-480

[58] J. F. Runckel, C. M. Willis e L. B. Salters Jr., Investigation of catalyst beds for 98%

concentration hydrogen peroxide, NASA Technical Note D-1808

[59] J. J. Rusek,New decomposition catalysts and characterization techniques for rocket-grade hydrogen peroxide, AIAA Paper 95-3087, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, USA, July 1995

[60] D. K. Huzel e D. H. Huang, Design of liquid-propellant rocket engines, Rocketdyne Division

of Rockwell International, 1992,

(5)

[61] N. Iarochenko e V. Dedic, Hydrogen peroxide as monopropellant - Catalysts and catalyst beds - Experience from more than thirty years of exploitation, 1st International Conference on Green Propellants for Space Propulsion, European Space Agency, Noordwijk, Holland, ISBN 92 9092-771-1, 2001

[62] C. R. Peterson e P. G. Hill, Mechanics and thermodynamics of propulsion, Addison-Wesley Publishing Company, 1992

[63] J. Ponzo, Small envelope, high ﬂux 90% hydrogen peroxide catalyst bed, AIAA Paper 2003- 4622, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2003

[64] E. Wernimont e G. Garboden, Performance of a 2500 lbf hydrogen peroxide-polyethylene hybrid, AIAA Paper 00-3545, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, July 2000

[65] E. Wernimont e G. Garboden, Experimentation with hydrogen peroxide oxidized rockets, AIAA Paper 99-2743, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, USA, June 1999

[66] E. Wernimont e M. Ventura, Catalyst bed testing for development of a 98% hydrogen peroxide procurement speciﬁcation, AIAA Paper 2002-3852, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, July 2002

[67] J. S. Mok, W. J. Helms, J. C. Sisco e W. E. Anderson, Decomposition and vaporization studies of hydrogen peroxide, AIAA Paper 2002-4028, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, July 2002

[68] T. E. Jacks e M. Beisler, Expanding hydrogen peroxide propulsion test capability at NASA’s Stennis space center E-complex, AIAA Paper 2003-5041, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, USA, June 1999

[69] Wong K., Derivation of the data reduction equations for the calibration of the six-components thrust stand in the CE-22 advanced nozzle test facility, NASA/TM 2003-212326, USA, April 2003

[70] R. M. Rivello, Theory and analysis of ﬂight structures, Mc Graw-Hill Book Comp., 1969 [71] Green hydrogen peroxide monopropellant rocket engine with advanced catalytic beds -

Technical, management and ﬁnancial proposal

[72] A. Cervone, A. J. Musker e C. Bramanti, Green hydrogen peroxide monopropellant rocket en- gine with advanced catalytic beds - Technical Notes 1&2, Energetica/DELTACAT Document n. ENER/TN01/H2O2

[73] A. Cervone, A. J. Musker e C. Bramanti, Green hydrogen peroxide monopropellant rocket en-

gine with advanced catalytic beds - Technical Notes 3&4, Energetica/DELTACAT Document

n. ENER/TN02/H2O2

(6)

[74] A. Cervone, A. J. Musker e L. Torre, Green hydrogen peroxide monopropellant rocket engine with advanced catalytic beds - Technical Notes 5&6, Energetica/DELTACAT Document n.

ENER/TN03/H2O2

[75] A. Pasini, L. Torre e A. J. Musker, Green hydrogen peroxide monopropellant rocket engine with advanced catalytic beds - Technical Notes 7&8, Energetica/DELTACAT Document n.

ENER/TN04/H2O2

[76] C. Bramanti, A. Cervone, L. Romeo, L. Torre, L. d’ Agostino, A. J. Musker e G. Saccoc- cia, Experimental characterization of advanced materials for the catalytic decomposition of hydrogen peroxide

[77] A. Cervone, L. Torre, L. d’ Agostino, A. J. Musker, G. T. Roberts, C. Bramanti e G.

Saccoccia, Development of hydrogen peroxide monopropellant rockets

[78] R. Parenti, Progetto di un banco di prova per endoreattori monopropellente a perossido d’

idrogeno, Tesi di laurea in Ingegneria Aerospaziale, Università di Pisa, Anno accademic 2003-2004

[79] A. Pasini, Progettazione e realizzazione di un impianto di prova per endoreattori a perossido

d’ idrogeno, Tesi di laurea in Ingegneria Aerospaziale, Università di Pisa, Anno accademic

2005-2006