Standard
Case breach fault model and diagnostic for the solid rocket. / Osipov, Viatcheslav V.
; Luchinsky, Dmitry G.; Smelyanskiy, Vadim N. et al.
Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2007. p. 8112-8125 (Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Vol. 8).
Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review
Harvard
Osipov, VV
, Luchinsky, DG, Smelyanskiy, VN & Timucin, DA 2007,
Case breach fault model and diagnostic for the solid rocket. in
Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, vol. 8, American Institute of Aeronautics and Astronautics, pp. 8112-8125, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United States,
8/07/07.
APA
Osipov, V. V.
, Luchinsky, D. G., Smelyanskiy, V. N., & Timucin, D. A. (2007).
Case breach fault model and diagnostic for the solid rocket. In
Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference (pp. 8112-8125). (Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Vol. 8). American Institute of Aeronautics and Astronautics.
Vancouver
Author
Bibtex
@inproceedings{f408769a32124c6a8a38ad1a5bcf22e6,
title = "Case breach fault model and diagnostic for the solid rocket",
abstract = "A model of the case breach fault for solid rocket boosters (SRBs) that takes into account burning-through hole in propellant, insulator and metal layers of a rocket case is developed. Melting of the metal layer and an ablation of the insulator layer in the presence of hot gas flow through the hole are analyzed in detail. Dynamics of the lateral (side) thrust produced by the growing hole is calculated for typical parameters of the SRB. A problem of inference of the fault parameters from the measurements of the nominal values of stagnation pressure and thrust is formulated and solved in quasi-steady approximation. An application of the recently developed Bayesian framework for diagnostics and prognostics of the case breach fault that can cause loss of flight control is discussed.",
author = "Osipov, {Viatcheslav V.} and Luchinsky, {Dmitry G.} and Smelyanskiy, {Vadim N.} and Timucin, {Dogan A.}",
year = "2007",
month = dec,
day = "10",
language = "English",
isbn = "1563479036",
series = "Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference",
publisher = "American Institute of Aeronautics and Astronautics",
pages = "8112--8125",
booktitle = "Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference",
note = "43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference ; Conference date: 08-07-2007 Through 11-07-2007",
}
RIS
TY - GEN
T1 - Case breach fault model and diagnostic for the solid rocket
AU - Osipov, Viatcheslav V.
AU - Luchinsky, Dmitry G.
AU - Smelyanskiy, Vadim N.
AU - Timucin, Dogan A.
PY - 2007/12/10
Y1 - 2007/12/10
N2 - A model of the case breach fault for solid rocket boosters (SRBs) that takes into account burning-through hole in propellant, insulator and metal layers of a rocket case is developed. Melting of the metal layer and an ablation of the insulator layer in the presence of hot gas flow through the hole are analyzed in detail. Dynamics of the lateral (side) thrust produced by the growing hole is calculated for typical parameters of the SRB. A problem of inference of the fault parameters from the measurements of the nominal values of stagnation pressure and thrust is formulated and solved in quasi-steady approximation. An application of the recently developed Bayesian framework for diagnostics and prognostics of the case breach fault that can cause loss of flight control is discussed.
AB - A model of the case breach fault for solid rocket boosters (SRBs) that takes into account burning-through hole in propellant, insulator and metal layers of a rocket case is developed. Melting of the metal layer and an ablation of the insulator layer in the presence of hot gas flow through the hole are analyzed in detail. Dynamics of the lateral (side) thrust produced by the growing hole is calculated for typical parameters of the SRB. A problem of inference of the fault parameters from the measurements of the nominal values of stagnation pressure and thrust is formulated and solved in quasi-steady approximation. An application of the recently developed Bayesian framework for diagnostics and prognostics of the case breach fault that can cause loss of flight control is discussed.
M3 - Conference contribution/Paper
AN - SCOPUS:36749038271
SN - 1563479036
SN - 9781563479038
T3 - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
SP - 8112
EP - 8125
BT - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics
T2 - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Y2 - 8 July 2007 through 11 July 2007
ER -
