Home > Research > Publications & Outputs > Diagnostics and prognostics for stage separatio...

Research

Links

Text available via DOI:

View graph of relations

Diagnostics and prognostics for stage separation failure

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

Published

Standard

Diagnostics and prognostics for stage separation failure. / Luchinsky, Dmitry G.; Hafiychu, Vasyl; Smelyanskiy, Vadim et al.
2011 Aerospace Conference, AERO 2011. IEEE, 2011. 5747595 (IEEE Aerospace Conference Proceedings).

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

Harvard

Luchinsky, DG, Hafiychu, V, Smelyanskiy, V, Hanson, JM, Hill, AD & Werkheiser, M 2011, Diagnostics and prognostics for stage separation failure. in 2011 Aerospace Conference, AERO 2011., 5747595, IEEE Aerospace Conference Proceedings, IEEE, 2011 IEEE Aerospace Conference, AERO 2011, Big Sky, MT, United States, 5/03/11. https://doi.org/10.1109/AERO.2011.5747595

APA

Luchinsky, D. G., Hafiychu, V., Smelyanskiy, V., Hanson, J. M., Hill, A. D., & Werkheiser, M. (2011). Diagnostics and prognostics for stage separation failure. In 2011 Aerospace Conference, AERO 2011 Article 5747595 (IEEE Aerospace Conference Proceedings). IEEE. https://doi.org/10.1109/AERO.2011.5747595

Vancouver

Luchinsky DG, Hafiychu V, Smelyanskiy V, Hanson JM, Hill AD, Werkheiser M. Diagnostics and prognostics for stage separation failure. In 2011 Aerospace Conference, AERO 2011. IEEE. 2011. 5747595. (IEEE Aerospace Conference Proceedings). doi: 10.1109/AERO.2011.5747595

Author

Luchinsky, Dmitry G. ; Hafiychu, Vasyl ; Smelyanskiy, Vadim et al. / Diagnostics and prognostics for stage separation failure. 2011 Aerospace Conference, AERO 2011. IEEE, 2011. (IEEE Aerospace Conference Proceedings).

Bibtex

@inproceedings{3fc28062b758430fb9bd93fa94f2e877,
title = "Diagnostics and prognostics for stage separation failure",
abstract = "An engineering assessment of the stage separation fault is reported for two-stage, vertically stacked space vehicle. The analysis combines explicit modeling of the fault evolution failure with analytical estimations based on simplifie physics-of-failure models. The following sequence of events is analyzed: (i) structural dynamics of the nozzle extension during the impact; (ii) yielding and burning through the damaged nozzle under the plume loading during engine start up; and (iii) reduction of the actual thrust and side load in the quasi-steady burning regime. The analysis reveals characteristic time-signatures of the impact-induced torque and lay down foundation for the development of a diagnosis and prognosis system for the stage separation fault.",
author = "Luchinsky, {Dmitry G.} and Vasyl Hafiychu and Vadim Smelyanskiy and Hanson, {John M.} and Hill, {Ashley D.} and Mary Werkheiser",
year = "2011",
month = may,
day = "13",
doi = "10.1109/AERO.2011.5747595",
language = "English",
isbn = "9781424473502",
series = "IEEE Aerospace Conference Proceedings",
publisher = "IEEE",
booktitle = "2011 Aerospace Conference, AERO 2011",
note = "2011 IEEE Aerospace Conference, AERO 2011 ; Conference date: 05-03-2011 Through 12-03-2011",

}

RIS

TY - GEN

T1 - Diagnostics and prognostics for stage separation failure

AU - Luchinsky, Dmitry G.

AU - Hafiychu, Vasyl

AU - Smelyanskiy, Vadim

AU - Hanson, John M.

AU - Hill, Ashley D.

AU - Werkheiser, Mary

PY - 2011/5/13

Y1 - 2011/5/13

N2 - An engineering assessment of the stage separation fault is reported for two-stage, vertically stacked space vehicle. The analysis combines explicit modeling of the fault evolution failure with analytical estimations based on simplifie physics-of-failure models. The following sequence of events is analyzed: (i) structural dynamics of the nozzle extension during the impact; (ii) yielding and burning through the damaged nozzle under the plume loading during engine start up; and (iii) reduction of the actual thrust and side load in the quasi-steady burning regime. The analysis reveals characteristic time-signatures of the impact-induced torque and lay down foundation for the development of a diagnosis and prognosis system for the stage separation fault.

AB - An engineering assessment of the stage separation fault is reported for two-stage, vertically stacked space vehicle. The analysis combines explicit modeling of the fault evolution failure with analytical estimations based on simplifie physics-of-failure models. The following sequence of events is analyzed: (i) structural dynamics of the nozzle extension during the impact; (ii) yielding and burning through the damaged nozzle under the plume loading during engine start up; and (iii) reduction of the actual thrust and side load in the quasi-steady burning regime. The analysis reveals characteristic time-signatures of the impact-induced torque and lay down foundation for the development of a diagnosis and prognosis system for the stage separation fault.

U2 - 10.1109/AERO.2011.5747595

DO - 10.1109/AERO.2011.5747595

M3 - Conference contribution/Paper

AN - SCOPUS:79955772099

SN - 9781424473502

T3 - IEEE Aerospace Conference Proceedings

BT - 2011 Aerospace Conference, AERO 2011

PB - IEEE

T2 - 2011 IEEE Aerospace Conference, AERO 2011

Y2 - 5 March 2011 through 12 March 2011

ER -