Top

Published in:

2021 | OriginalPaper | Chapter

2. The Thrust Chamber Assembly

Author : Alessandro de Iaco Veris

Published in: Fundamental Concepts of Liquid-Propellant Rocket Engines

Publisher: Springer International Publishing

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

search-config

AI-assisted search

Off

Abstract

The principal components, i.e., the combustion chamber and the nozzle, of the thrust chamber of a rocket engine are presented and discussed together with their performance parameters. Injectors, engine cycles, and igniters are discussed. Methods are given for their quantitative design. Cooling systems and combustion stabilising devices are also presented.

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!

inform now

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!

inform now

previous chapter Fundamental Concepts on Liquid-Propellant Rocket Engines

next chapter Feed Systems Using Gases Under Pressure

West J, Westra D, Richardson BR, Tucker PK (2014) Designing liquid rocket engine injectors for performance, stability, and cost. In: Conference paper. NASA Marshall Space Flight Centre, 16 Nov 2014, 13 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20150002585.pdf

Sutton GP, Biblarz O (2001) Rocket propulsion elements. 7th edn, Wiley, New York. ISBN 0-471-32642-9

NASA (2015) Space Travel, NASA Tests Methane-Powered Engine Components for Next Generation Landers. Marshall Space Flight Centre, 28 Oct 2015. https://www.nasa.gov/sites/default/files/thumbnails/image/img_3190.jpg

Tomazic WA, Bartoo ER, Rollbuhler RJ (1960) Experiments with hydrogen and oxygen in regenerative engines at chamber pressures from 100 to 300 pounds per square inch absolute. NASA TM X-253, 1st Apr 1960, 37 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660024054.pdf

Huzel DK, Huang DH (1967) Design of liquid propellant rocket engines. NASA SP-125, NASA. 2nd edn Washington, D.C., 472 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710019929.pdf

Bilstein RE (1996) Stages to Saturn. NASA SP-4206. https://ia802605.us.archive.org/19/items/stagestosaturnte00bilsrich/stagestosaturnte00bilsrich.pdf

NASA, Math and science at work, space shuttle roll maneuver student edition. http://www.nasa.gov/pdf/519348main_AP_ST_Phys_RollManeuver.pdf

NASA. https://spaceflightsystems.grc.nasa.gov/education/rocket/rktth1.html

NASA. http://exploration.grc.nasa.gov/education/rocket/rktcontrl.html

10.

NASA. http://www.hq.nasa.gov/office/pao/History/conghand/orient.htm

11.

Edwards SS, Parker GH (1958) An investigation of the jetevator as a means of thrust vector control. LMSD-2630, Lockheed, Sunnyvale, California, USA, Feb 1958, 44 p. http://www.dtic.mil/dtic/tr/fulltext/u2/a950112.pdf

12.

Spinardi G (1994) From Polaris to trident: the development of US fleet ballistic missile technology. Cambridge University Press. ISBN 0-521-41357-5

13.

NASA dryden fact sheet—highly manoeuvrable aircraft technology. http://www.nasa.gov/sites/default/files/images/110536main_HiMAT_3-view.jpg

14.

Benson T (ed) Practical rocketry, NASA, Glenn research centre. http://exploration.grc.nasa.gov/education/rocket/TRCRocket/practical_rocketry.html

15.

McGlinchey LF (1974) Viking orbiter 1975 thrust vector control system accuracy. NASA-CR-140705, JPL Technical Memorandum 33–703, 15 Oct 1974. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750002097.pdf

16.

NASA Space Science Data Coordinated Archive, Viking 1 Orbiter. https://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=1975-075A

17.

NASA (1968) Saturn V news reference, J-2 engine fact sheet, Dec 1968. https://www.nasa.gov/centers/marshall/pdf/499245main_J2_Engine_fs.pdf

18.

NASA. Beginner’s guide to rockets, guidance system. https://spaceflightsystems.grc.nasa.gov/education/rocket/guidance.html

19.

Noll RB, Zvara J, Deyst JJ (1971) Spacecraft attitude control during thrusting manoeuvres, NASA SP-8059, Feb 1971, 51 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710016722.pdf

20.

Shamnas MS, Balakrishnan SR, Balaji S (2013) Effects of secondary injection in rocket nozzle at various conditions. Int J Eng Res Technol (IJERT) 2(6):373–379

21.

Anonymous (1946) Augmented flow—an interesting method of fluid-flow augmentation with attractive possibilities. Flight, 15 Aug 1946, pp 174–175

22.

Blake BA (2009) Numerical investigation of fluidic injection as a means of thrust modulation. Final thesis report, 2009, School of Engineering and Information Technology, University of New South Wales at the Australian Defence Force Academy, Canberra, Australia, 29 p. Article available at the http://seit.unsw.adfa.edu.au/ojs/index.php/juer/article/viewFile/256/155

23.

Strykowski PJ, Krothapalli A, Forliti DJ (1996) Counterflow thrust vectoring of supersonic jets. AIAA J 34(11):2306–2314

24.

Hunter CA, Deere KA (1999) Computational investigation of fluidic counterflow thrust vectoring, AIAA 99-2669. In: 35th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, Los Angeles, CA, 20–23 June 1999, 13 p

25.

Deere KA, Berrier BL, Flamm JD, Johnson SK (2003) Computational study of fluidic thrust vectoring using separation control in a nozzle, AIAA-2003-3803. In: 21st AIAA applied aerodynamics conference, 23–26 June 2003, Orlando, Florida, USA, 11 p

26.

Wing DJ, Giuliano VJ (1997) Fluidic thrust vectoring of an axisymmetric exhaust nozzle at static conditions, FEDSM97-3228. In: 1997 ASME fluids engineering division summer meeting, 22–26 June 1997, 6 p

27.

Heppenheimer TA (1999) The space shuttle decision: NASA search for a reusable space vehicle. NASA SP-4221. 1999, 554 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990056590.pdf

28.

Hyde JC, Gill GS (1976) Liquid rocket engine nozzles, NASA SP-8120. NASA, Washington, D.C., July 1976, 123 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19770009165.pdf

29.

Crown JC (1948) Supersonic nozzle design. NACA Technical Note No. 1651, NACA, Washington, D.C., June 1948, 35 p https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930082268.pdf

30.

Rao GVR (1958) Exhaust nozzle contour for optimum thrust. J Jet Propul 28(6):377–382

31.

Kuo KK, Acharya R (2012) Applications of turbulent and multiphase combustion. Wiley, Hoboken, New Jersey. ISBN 978-1-118-12756-8

32.

Ahlberg JH, Hamilton S, Migdal D, Nilson EN (1961) Truncated perfect nozzles in optimum nozzle design. ARS J 31(5):614–620CrossRef

33.

Rao GVR (1960) Approximation of optimum thrust nozzle contour. ARS J 30(6):581

34.

Braeunig RA, Rocket and space technology—rocket propulsion. http://braeunig.us/space/propuls.htm

35.

Newlands R (2017) The thrust optimised parabolic nozzle. Aspirespace, 18 Apr 2017. http://www.aspirespace.org.uk/downloads/Thrust%20optimised%20parabolic%20nozzle.pdf

36.

Aukerman CA (1991) Plug nozzles—the ultimate customer driven propulsion system. NASA-CR-187169, Aug 1991, 27 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920013861.pdf

37.

Corda S, Neal BA, Moes TR, Cox TH, Monaghan RC, Voelker LS, Corpening GP, Larson RR, Powers BG (1998) Flight testing the linear aerospike SR-71 experiment (LASRE), NASA/TM-1998-206567. NASA Dryden Space Research Centre, Sept 1998, 26 p. https://www.nasa.gov/centers/dryden/pdf/88598main_H-2280.pdf

38.

NASA. Linear aerospike SR-71 experiment (LASRE) Project. https://www.nasa.gov/centers/armstrong/news/FactSheets/FS-043-DFRC.html

39.

NASA. https://www.hq.nasa.gov/pao/History/x-33/xrs2200.htm

40.

Anonymous (1981) Liquid rocket propulsion technology: an evaluation of NASA’s program, NASA-CR-164550, Jan 1981, 67 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810018653.pdf

41.

Shyne RJ, Keith Th G Jr (1990) Analysis and design of optimised truncated scarfed nozzles subject to external flow field effects. NASA Technical Memorandum 105175, Jan 1990, 12 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015790.pdf

42.

O’Leary RA, Beck JE (1992) Nozzle design, Threshold, Pratt & Whitney Rocketdyne’s engineering journal of power technology. Spring 1992. http://www.rocket-propulsion.info/resources/articles/NozzleDesign.pdf

43.

Wieseneck HC (1970) Regenerative cooling of the space shuttle engine. NASA, July 1970, 32 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19700030313.pdf

44.

Turner MJL (2006) Rocket and spacecraft propulsion, 2nd edn. Springer, Berlin. ISBN 3-540-22190-5

45.

Van Huff NE, Fairchild DA (1972) Liquid rocket engine fluid-cooled combustion chambers. NASA SP-8087, Apr 1972, 120 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19730022965.pdf

46.

Bartz DR (963) Turbulent boundary-layer heat transfer from rapidly accelerating flow of rocket combustion gases and of heated air, NASA CR-62615. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California. USA, Dec 1963, 128 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650013685.pdf

47.

Hill PhG, Peterson CR (1965) Mechanics and thermodynamics of propulsion, addison-wesley, reading. USA, Massachusetts

48.

Wang Q, Wu F, Zeng M, Luo L, Sun, J (2006) Numerical simulation and optimization on heat transfer and fluid flow in cooling channel of liquid rocket engine thrust chamber. Eng Comput 23(8):907–921

49.

Harrje DT, Reardon FH (ed) (1972) Liquid propellant rocket combustion instability. NASA SP-194, Jan 1972, 657 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720026079.pdf

50.

Anonymous (1998) Space Shuttle main engine orientation. Boeing-Rocketdyne Propulsion & Power, Presentation BC98-04, June 1998, 105 p. http://large.stanford.edu/courses/2011/ph240/nguyen1/docs/SSME_PRESENTATION.pdf

51.

Anonymous (1993) Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. NASA-CR-193949, 16 Nov 1993, 169 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940019998.pdf

52.

Taler D, Taler J (2017) Simple heat transfer correlations for turbulent tube flow. In: E3S Web of conferences 13, 02008 (2017), 7 pages. https://www.e3s-conferences.org/articles/e3sconf/pdf/2017/01/e3sconf_wtiue2017_02008.pdf

53.

Gnielinski V (1975) Neue Gleichungen für den Wärme- und den Stoffübergang in turbulent durchströmten Rohren und Kanälen. Forsch Ingenieurwes 41:8–16

54.

Giovanetti AJ, Spadaccini LJ, Szetela EJ (1983) Deposit formation and heat transfer in hydrocarbon rocket fuels. NASA-CR-168277, 1983, 168 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840004157.pdf

55.

Haidn OJ (2008) Advanced rocket engines. In: Advances on propulsion technology for high-speed aircraft, NATO RTO-EN-AVT-150, 2008, Neuilly-sur-Seine (France), 40 p. Available at the http://www.macro-inc.com/NASADocs/AdvanceRocketEnginesEN-AVT-150-06.pdf

56.

Locke JM, Landrum DB (2008) Study of heat transfer correlations for supercritical hydrogen in regenerative cooling channels. J Propul Power 24(1):94–103

57.

Sloop JL (1978) Liquid hydrogen as a propulsion fuel. 1945-1959, NASA SP-4404, Jan 1978, 341 p. Available at the https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790008823.pdf

58.

Colebrook CF (1939) Turbulent flow in pipes, with particular reference to the transition region between smooth and rough pipe laws. J Inst Civil Eng 11(4):133–156

59.

Nuclear Power, Darcy Friction Factor, Relative Roughness of Pipe. http://www.nuclear-power.net/nuclear-engineering/fluid-dynamics/major-head-loss-friction-loss/relative-roughness-of-pipe/

60.

AJ Design Software, Colebrook Equations Formulas Calculator. https://www.ajdesigner.com/php_colebrook/colebrook_equation.php

61.

Special Metals Corporation, Inconel^® alloy 718, Pub. No. SMC-045. http://www.specialmetals.com/assets/smc/documents/inconel_alloy_718.pdf

62.

National Institute of Standards and Technology (NIST), NIST Chemistry WebBook, SRD 69, Hydrogen. http://webbook.nist.gov/cgi/cbook.cgi?ID=C1333740&Mask=4, see also Thermophysical Properties of Fluid Systems. https://webbook.nist.gov/chemistry/fluid/

63.

Stenholm T, Pekkari LO, Andersson T (1988) The development of the Vulcain nozzle extension. In: 34th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, 13–15 July 1988, Cleveland, Ohio, USA

64.

Rydén R, Johansson L, Palmnäs U (2004) The Volvo Aero laser welded sandwich nozzle for booster engines. In: 55th International Astronautical Congress 2004—Vancouver, Canada, Paper number IAC-04-S.3.07. https://iafastro.directory/iac/archive/browse/IAC-04/S/3/1259/

65.

Lucas JG, Golladay RL (1963) An experimental investigation of gaseous-film cooling of a rocket motor. NASA TN D-1988, Oct 1963, 24 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19630012015.pdf

66.

Zucrow MJ, Sellers JP (1961) Experimental investigation of rocket motor film cooling. ARS J 668

67.

Hatch JE, Papell SS (1959) Use of a theoretical flow model to correlate data for film cooling or heating an adiabatic wall by tangential injection of gases of different fluid properties. NASA TN D-130, Nov 1959, 44 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068390.pdf

68.

Hannum N, Roberts WE, Russell LM (1977) Hydrogen film cooling of a small hydrogen-oxygen thrust chamber and its effect on erosion rates of various ablative materials. NASA-TP-1098, Dec 1977, 29 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19780005181.pdf

69.

Eckert ERG, Livingood JNB (1954) Comparison and effectiveness of convection-, transpiration-, and film-cooling methods with air as a coolant. NACA-TR-1182, Jan 1954, 17 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930092205.pdf

70.

Rannie W (1947) A simplified theory for porous wall cooling. Progress Report No. 4–50, Jet Propulsion Laboratory, Pasadena, California, USA., 25 Nov 1947, 24 p. https://trs.jpl.nasa.gov/bitstream/handle/2014/45706/17-0944.pdf?sequence=1&isAllowed=y

71.

Ewen RL, Evensen HM (1977) Liquid rocket engine self-cooled combustion chambers. NASA SP-8124, Sept 1977, 130 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19780013268.pdf

72.

Reed BD, Biaglow JA, Schneider SJ (1997) Iridium-coated rhenium radiation-cooled rockets, NASA TM-107453, July 1997, 14 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19970036365.pdf

73.

National Institute of Standards and Technology (NIST). https://physics.nist.gov/cgi-bin/cuu/Value?sigma

74.

Combs LP et al (1974) Liquid rocket engine combustion stabilisation devices. NASA SP-8113, Nov 1974, 127 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750020175.pdf

75.

Gill GS, Nurick WH, Keller RB Jr (ed) Liquid rocket engine injectors. NASA SP-8089, Mar 1976, 130 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19760023196.pdf

76.

Casiano MJ, Hulka JR, Yang V (2010) Liquid-propellant rocket engine throttling: a comprehensive review. J Propu Power 26(5):897–923. http://www.yang.gatech.edu/publications/Journal/JPP%20(2010,%20Casiano).pdf

77.

Hammock WR Jr, Currie EC, Fisher AE (1973) Apollo experience report—descent propulsion system. NASA TN D-7143, Mar 1973, 36 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19730011150.pdf

78.

Wikipedia, SpaceX rocket engines. https://en.wikipedia.org/wiki/SpaceX_rocket_engines

79.

Stangeland ML (1988) Turbopumps for liquid rocket engines, Threshold, Pratt & Whitney Rocketdyne’s engineering journal of power technology, Summer 1988. http://www.pwrengineering.com/articles/turbopump.htm

80.

Macaluso SB, Keller RB Jr (ed) (1974) Liquid rocket engine turbines. NASA SP-8110, Jan 1974, 160 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740026132.pdf

81.

Greene WD, Inside the J-2X doghouse: the gas-generator cycle engine. NASA. https://blogs.nasa.gov/J2X/tag/gas-generator/

82.

Sobin AJ, Bissel WR, Keller RB Jr (ed) (1974) Turbopump systems for liquid rocket engines. NASA SP-8107, Aug 1974, 168 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750012398.pdf

83.

Zehetner HW, Keller RB Jr. (ed) Liquid propellant gas generators. NASA SP-8081, Mar 1972, 110 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19730018978.pdf

84.

Kosanke KL, Kosanke BJ, Pyrotechnic ignition and propagation: a review. In: Kosanke KL, Kosanke BJ (eds) Selected pyrotechnic publications of, pp 420–431. http://www.jpyro.com/wp-content/uploads/2012/08/Kos-420-431.pdf

85.

Barrett DH, Keller RB Jr (ed) (1971) Solid rocket motor igniters. NASA SP-8051, Mar 1971, 112 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710020870.pdf

86.

Kosanke KL, Kosanke BJ (2012) Electric matches and squibs. In: KL Kosanke, BJ Kosanke (eds) Selected pyrotechnic publications of, pp. 257–259. http://www.jpyro.com/wp-content/uploads/2012/08/Kos-257-259.pdf

87.

United Launch Alliance. http://www.ulalaunch.com/uploads/docs/AtlasVUsersGuide2010.pdf, Public Domain. https://commons.wikimedia.org/w/index.php?curid=48196878

88.

Clark JD (1972) Ignition!: an informal history of liquid rocket propellants. Rutgers University Press, New Brunswick, New Jersey. ISBN 0-8135-0725-1

89.

Hulka J, Forde JS, Werling RE, Anisimov VS, Kozlow VA, Kositsin IP (1998) Modification and verification testing of a Russian NK-33 rocket engine for reusable and restartable applications. AIAA 98-3361, 1998, 26 p. http://lpre.de/resources/articles/AIAA-1998-3361.pdf

90.

Greene WD (2014) Inside the LEO doghouse: light my fire!. NASA, 24 Feb 2014. https://blogs.nasa.gov/J2X/tag/ignition/

91.

Kleinhenz J, Sarmiento Ch, Marshall W (2012) Experimental investigation of augmented spark ignition of a LO₂/LCH₄ reaction control engine at altitude conditions. NASA/TM-2012-217611, June 2012, 43 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120011145.pdf

92.

Anderson WE, Butler K, Crocket D, Lewis T, McNeal C (2000) Peroxide propulsion at the turn of the century, 13 Mar 2000, 59 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20000033615.pdf

93.

Prentiss SS (1956) Safety device, including fusible member for rocket engine starting control, U.S. patent No. 2,741,085 granted on the 10th of Apr 1956. https://patents.google.com/patent/US2741085

94.

Rayleigh L (1878) The theory of sound, vol 2. Macmillan & Co., London. http://gallica.bnf.fr/ark:/12148/bpt6k95131k.image

95.

Burrows MC, Exploring in aerospace rocketry, 4—Thermodynamics, NASA TM X-52391, Jan 1968, 21 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19680010371.pdf

96.

Ellison LR, Moser MD, Combustion instability analysis and the effect of drop size on acoustic driving rocket flow, 13 May 2004, 6 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20040075603.pdf

97.

Wikipedia, by Loungeflyz (CC BY-SA 4.0. https://creativecommons.org/licenses/by-sa/4.0) from Wikimedia Commons

98.

Jonash ER, Tomazic WA (1962) Current research and development on thrust chambers. In: Proceedings of the NASA-university conference on the science and technology of space exploration, vol 2. NASA SP-11, Chicago, Illinois, 1–3 Nov 1962, pp. 43–52. http://www.dtic.mil/dtic/tr/fulltext/u2/a396443.pdf

99.

Frendi A, Nesman T, Canabal F (2005) Control of combustion instabilities through various passive devices, NASA, 25 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20050182054.pdf

100.

Kinsler LE, Frey AR, Coppens AB, Sanders JV (2000) Fundamentals of acoustics. 4th edn, Wiley, New York. ISBN 0-471-84789-5

101.

Rubin S, Prevention of coupled structure-propulsion instability (pogo). NASA SP-8055, Oct 1970, 52 p. https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19710016604.pdf

102.

Modlin T, Space Shuttle pogo—NASA eliminates “bad vibrations”. Eng Innov Struct Des 270–285 https://www.nasa.gov/centers/johnson/pdf/584733main_Wings-ch4g-pgs270-285.pdf

Title: The Thrust Chamber Assembly
Author: Alessandro de Iaco Veris
Publisher: Springer International Publishing
Book: Fundamental Concepts of Liquid-Propellant Rocket Engines
Print ISBN: 978-3-030-54703-5

Electronic ISBN: 978-3-030-54704-2

Copyright Year: 2021
DOI: https://doi.org/10.1007/978-3-030-54704-2_2

Springer Professional

Abstract

Please log in to get access to your license.

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

Springer Professional "Wirtschaft+Technik"

Springer Professional "Technik"

Premium Partner