Skip to main content

2011 | OriginalPaper | Buchkapitel

28. Pintle Injectors

verfasst von : S. D. Heister

Erschienen in: Handbook of Atomization and Sprays

Verlag: Springer US

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

Pintle injectors have been developed for applications in rocket propulsion, but could potentially have high flowrate in other applications due to their relative simplicity. The spray from a pintle injector is formed from the collision of radial jets of fluid issuing from the center of the pintle post with an annular sleeve of fluid travelling axially along the post. The resultant interactions produce a conical spray similar to a hollow cone swirl atomizer. This chapter reviews historical applications of pintle injectors and theoretical bases for their design.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

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!

Fußnoten
1
Hypergolic propellants react/combust spontaneously upon contact thereby eliminating the need for a separate ignition system.
 
Literatur
1.
Zurück zum Zitat Dressler, G.A. and Bauer, J.M., TRW Pintle Engine Heritage and Performance Characteristics, AIAA 2000-3871, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000. Dressler, G.A. and Bauer, J.M., TRW Pintle Engine Heritage and Performance Characteristics, AIAA 2000-3871, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000.
2.
Zurück zum Zitat Escher, D.W., Design and Preliminary Hot Fire and Cold Flow Testing of Pintle Injectors, MS thesis, Mechanical Engineering, The Pennsylvania State University, December 1996. Escher, D.W., Design and Preliminary Hot Fire and Cold Flow Testing of Pintle Injectors, MS thesis, Mechanical Engineering, The Pennsylvania State University, December 1996.
3.
Zurück zum Zitat Siegel, B., Research of Low-Thrust Bipropellant Engines, Independent Research Program Annual Report, 1961, #9990-6020-RU-000, pp. VI-59 to VI-73, Space Technology Laboratories, Inc., Redondo Beach 1961. Siegel, B., Research of Low-Thrust Bipropellant Engines, Independent Research Program Annual Report, 1961, #9990-6020-RU-000, pp. VI-59 to VI-73, Space Technology Laboratories, Inc., Redondo Beach 1961.
4.
Zurück zum Zitat Elverum, G., Staudhammer, P., Miller, J., Hoffman, A., and Rockow, R., The Descent Engine for the Lunar Module, AIAA 67-521, AIAA 3rd Propulsion Joint Propulsion Specialist Conference, July 1967. Elverum, G., Staudhammer, P., Miller, J., Hoffman, A., and Rockow, R., The Descent Engine for the Lunar Module, AIAA 67-521, AIAA 3rd Propulsion Joint Propulsion Specialist Conference, July 1967.
5.
Zurück zum Zitat Gilroy, R. and Sackheim, R., The Lunar Module Descent Engine – A Historical Perspective, AIAA 89-2385, 25th AIAA/SAE/ASME Joint Propulsion Conference, 1989. Gilroy, R. and Sackheim, R., The Lunar Module Descent Engine – A Historical Perspective, AIAA 89-2385, 25th AIAA/SAE/ASME Joint Propulsion Conference, 1989.
6.
Zurück zum Zitat Dressler, G.A., Summary of Deep Throttling Rocket Engines with Emphasis on Apollo LMDE, AIAA 2006-5220, 42nd AIAA Joint Propulsion Conference, Sacramento, 2006. Dressler, G.A., Summary of Deep Throttling Rocket Engines with Emphasis on Apollo LMDE, AIAA 2006-5220, 42nd AIAA Joint Propulsion Conference, Sacramento, 2006.
7.
Zurück zum Zitat Calvignac, J., Design and Testing of a Non-Toxic 870-LBf Engine, AIAA 2000-3851, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000. Calvignac, J., Design and Testing of a Non-Toxic 870-LBf Engine, AIAA 2000-3851, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000.
8.
Zurück zum Zitat Austin, B., Matthews, J., and Heister, S.D., Engine/Injector Development for New Nontoxic, Storable, Hypergolic Bipropellants, 13th Propulsion Engineering Research Center Annual Symposium on Propulsion, Huntsville, 2001. Austin, B., Matthews, J., and Heister, S.D., Engine/Injector Development for New Nontoxic, Storable, Hypergolic Bipropellants, 13th Propulsion Engineering Research Center Annual Symposium on Propulsion, Huntsville, 2001.
9.
Zurück zum Zitat Austin, B., Heister, S.D., and Anderson, W.A., Development of Pintle and Splashplate Injectors for Nontoxic, Storable, Hypergolic Bipropellants, Journal of Propulsion and Power, 21(4), 627–635, 2005.CrossRef Austin, B., Heister, S.D., and Anderson, W.A., Development of Pintle and Splashplate Injectors for Nontoxic, Storable, Hypergolic Bipropellants, Journal of Propulsion and Power, 21(4), 627–635, 2005.CrossRef
11.
Zurück zum Zitat Heister, S.D., Nguyen, T.T., and Karagozian, A.R., Modeling of Liquid Jets Injected Transversely into a Supersonic Crossflow, AIAA Journal, 27(12), 1727–1734, 1989.CrossRef Heister, S.D., Nguyen, T.T., and Karagozian, A.R., Modeling of Liquid Jets Injected Transversely into a Supersonic Crossflow, AIAA Journal, 27(12), 1727–1734, 1989.CrossRef
12.
Zurück zum Zitat Austin, B.J., Development of a Pintle-Based Engine for Nontoxic Hypergolic Propellants, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2002. Austin, B.J., Development of a Pintle-Based Engine for Nontoxic Hypergolic Propellants, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2002.
13.
Zurück zum Zitat Fritz, D., Dressler, G., Mayer, N., and Johnson, L., Development and Flight Qualification of the Propulsion and Reaction Control System for ERIS, 28th AIAA 92-3663, AIAA/SAE/ASME/ASEE Joint Propulsion Conference, July 1992. Fritz, D., Dressler, G., Mayer, N., and Johnson, L., Development and Flight Qualification of the Propulsion and Reaction Control System for ERIS, 28th AIAA 92-3663, AIAA/SAE/ASME/ASEE Joint Propulsion Conference, July 1992.
14.
Zurück zum Zitat Fritz, D. and Gavitt, K., Gel Propulsion for the Fourth Generation Escape System, Paper presented at the 1993 SAFE Symposium, Las Vegas, November 1993. Fritz, D. and Gavitt, K., Gel Propulsion for the Fourth Generation Escape System, Paper presented at the 1993 SAFE Symposium, Las Vegas, November 1993.
15.
Zurück zum Zitat Dressler, G., Stoddard, F., Gavitt, K., and Klem, M., Test Results from a Simple, Low-Cost Pressure-Fed Liquid Hydrogen/Liquid Oxygen Rocket Combustor, 1993 JANNAF Propulsion Meeting, November 1993, CPIA Pub. 602, Vol. II, pp. 51–67. Dressler, G., Stoddard, F., Gavitt, K., and Klem, M., Test Results from a Simple, Low-Cost Pressure-Fed Liquid Hydrogen/Liquid Oxygen Rocket Combustor, 1993 JANNAF Propulsion Meeting, November 1993, CPIA Pub. 602, Vol. II, pp. 51–67.
16.
Zurück zum Zitat Hodge, K., Crofoot, T., and Nelson, S., Gelled Propellants for Tactical Missile Applications, AIAA 99-2976, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, June 1999. Hodge, K., Crofoot, T., and Nelson, S., Gelled Propellants for Tactical Missile Applications, AIAA 99-2976, 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, June 1999.
17.
Zurück zum Zitat Gavitt, K. and Mueller, T., TRW LCPE 650 Klbf LOX/LH2 Test Results, AIAA 2000-3853, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2000. Gavitt, K. and Mueller, T., TRW LCPE 650 Klbf LOX/LH2 Test Results, AIAA 2000-3853, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 2000.
18.
Zurück zum Zitat Klem, M.D. and Stoddard, F.J., Results of 178 kN (40,00 lbf) Thrust LOX/LH2 Pintle Injector Engine Tests, JANNAF CS/PSH/EPTS/SPIRITS Joint Meeting, Huntsville, October 1995. Klem, M.D. and Stoddard, F.J., Results of 178 kN (40,00 lbf) Thrust LOX/LH2 Pintle Injector Engine Tests, JANNAF CS/PSH/EPTS/SPIRITS Joint Meeting, Huntsville, October 1995.
19.
Zurück zum Zitat Klem, M.D., Jankovsky, A.L., and Stoddard, F.J., Results of LOX/RP-1 Pintle Injector Engine Tests, JANNAF CS/PSH/EPTS/SPIRITS Joint Meeting, Huntsville, October 1995. Klem, M.D., Jankovsky, A.L., and Stoddard, F.J., Results of LOX/RP-1 Pintle Injector Engine Tests, JANNAF CS/PSH/EPTS/SPIRITS Joint Meeting, Huntsville, October 1995.
20.
Zurück zum Zitat Mueller, T. and Dressler, G., TRW 40 KLBf LOX/RP-1 Low Cost Pintle Engine Test Results, AIAA 2000-3863, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000. Mueller, T. and Dressler, G., TRW 40 KLBf LOX/RP-1 Low Cost Pintle Engine Test Results, AIAA 2000-3863, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, July 2000.
21.
Zurück zum Zitat Kim, P.Y., Majmaki, A., Papesh, C., Schneider, D., Thompson, M., and Weinstock, V.D., Design and Development Testing of TR108 – a 30Klbf Thrust-Class Hydrogen Peroxide/Hydrocarbon Pump-Fed Engine, AIAA 2005-3566, 41st AIAA Joint Propulsion Conference, Tuscon, 2005. Kim, P.Y., Majmaki, A., Papesh, C., Schneider, D., Thompson, M., and Weinstock, V.D., Design and Development Testing of TR108 – a 30Klbf Thrust-Class Hydrogen Peroxide/Hydrocarbon Pump-Fed Engine, AIAA 2005-3566, 41st AIAA Joint Propulsion Conference, Tuscon, 2005.
Metadaten
Titel
Pintle Injectors
verfasst von
S. D. Heister
Copyright-Jahr
2011
Verlag
Springer US
DOI
https://doi.org/10.1007/978-1-4419-7264-4_28

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.