Skip to main content
Log in

Role of Metallographic Analysis in the Identification of Location of Crack Initiation in a Burst Tested AA 2219 Propellant Tank

  • Technical Article
  • Published:
Metallography, Microstructure, and Analysis Aims and scope Submit manuscript

Abstract

Owing to its excellent combination of weldability and strength at low temperatures (up to 4 K), aluminum alloy AA 2219 is the material of choice for the design of propellant tanks for cryogenic engines of satellite launch vehicles. In order to assess the design margins available, one propellant tank has been subjected to burst test. This paper highlights the role of microstructural analysis conducted on the burst tested propellant tank in locating the origin of crack initiation. Specimens collected from different locations of the burst tested tank have been subjected to optical microscopy and scanning electron microscopy to locate the origin of crack initiation.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16

Similar content being viewed by others

References

  1. A.K. Jha, S.V.S. Narayana Murty, K. Sreekumar, P.P. Sinha, High strain rate deformation and cracking of AA 2219 aluminium alloy welded propellant tank. Eng. Fail. Anal. 16, 2209–2216 (2009)

    Article  Google Scholar 

  2. A.K. Jha, N. Shiresha, S.V.S. Narayana Murty, V. Diwakar, K. Sreekumar, Ballistic impact testing of AA2219 aluminium alloy welded plates and their metallurgical characterisation. Indian J. Eng. Mater. Sci. 12, 221–226 (2005)

    Google Scholar 

  3. C.F. Tiffany, P.M. Lorenz, Compatibility of tankage materials with liquid propellants, AD0853957, Boeing Company Space Division, Seattle

  4. ASM, ASM Speciality Metals Hand Book on Aluminium Alloys (American Society for Metals, Materials Park, OH, 2003)

    Google Scholar 

  5. M. Swathi Kiranmayee, A.K. Jha, A.K. Manwatkar, P. Ramesh Narayanan, K. Sreekumar, P.P. Sinha, Microstructural Characterisation of AA2219 Weldments. Mater. Sci. Forum 710, 638–643 (2012)

    Article  Google Scholar 

  6. S. Malarvizhi, K. Raghukandan, N. Viswanathan, Effect of post weld aging treatment on tensile properties of electron beam welded AA2219 aluminum alloy. Int. J. Adv. Manuf. Technol. 37, 294–301 (2008)

    Article  Google Scholar 

  7. G.J. Lal, P. Jayesh, K. Thyagarajan, Burst pressure estimation of reworked nozzle weld on spherical domes. Indian J. Eng. Mater. Sci. 21, 88–92 (2014)

    Google Scholar 

  8. M. Windisch, D.Z. Sun, D. Memhard, D. Siegele, Defect tolerance assessment of ARIANE 5 structures on the basis of damage mechanics material modelling. Eng. Fract. Mech. 76, 59–73 (2009)

    Article  Google Scholar 

  9. V.L. Hutchinson, Jr., J.R. Olds, in Estimation of Launch Vehicle Propellant Tank Structural Weight Using Simplified Beam Approximation.AIAA 2004-3661, 40th IAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit Fort Lauderdale, Florida July 11–14, 2004

  10. A.H. Taylor, L.R. Jackson, Analytical study of reusable flight-weight cryogenic propellant tank designs. J. Space Craft 23, 149–157 (1986)

    Article  Google Scholar 

  11. B.P. Kashyap, K. Tangri, Evidence for cavitation during superplastic deformation of an Al-Cu eutectic alloy. Scr. Metall. 20, 769–771 (1986)

    Article  Google Scholar 

  12. A.K. Shukla, R. Suresh Kumar, S.V.S. Narayana Murty, K. Mondal, Enhancement of high temperature ductility of hot-pressed Cu–Cr–Nb alloy by hot rolling. Mater. Sci. Eng. A577, 36–42 (2013)

    Article  Google Scholar 

Download references

Acknowledgments

Authors sincerely wish to thank the designers of the tank, structural testing team at INSTEF, VSSC. They wish to thank Project Director, LVM3 project for his kind support. They wish to thank the Director, VSSC for granting permission to publish this work.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to S. V. S. Narayana Murty.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Murty, S.V.S.N., Manwatkar, S.K. & Narayanan, P.R. Role of Metallographic Analysis in the Identification of Location of Crack Initiation in a Burst Tested AA 2219 Propellant Tank. Metallogr. Microstruct. Anal. 4, 392–402 (2015). https://doi.org/10.1007/s13632-015-0223-3

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s13632-015-0223-3

Keywords

Navigation