Combat survivability of hit aircraft

• Autorzy: Woch M. , Bońkowski T. , Kłysz S.
• Języki publikacji: EN

Abstrakty

EN

The paper is provides a preliminary breakdown susceptibility analysis for an aircraft PZL-130 ORLIK TC II in combat conditions. An analysis of breakdown forms and consequences for aircraft sections and installations in battle conditions including probability of being shot down when hit was made. The article presents a theoretical outline for calculation methods on aircraft kill probability in case of being shot, depending on critical element configuration and number of hits. The probability figures have been calculated for a specific model describing the aircraft PZL-130 ORLIK TC II. As a result of the conducted analysis it was possible to determine, for a specified weapon caliber, probabilities and effects of receiving combat damage.

Słowa kluczowe

EN

pzl-130 orlik; survivability analysis; risk; safety

• Wydawca: Polskie Towarzystwo Bezpieczeństwa i Niezawodności
• Czasopismo: Journal of Polish Safety and Reliability Association
• Rocznik: 2013
• Tom: Vol. 4, No. 2
• Strony: 267--272
• Opis fizyczny: Bibliogr. 11 poz., rys., tab., wykr.

Twórcy

autor

Woch M.

• Warsaw University of Technology, Warsaw, Poland

autor

Bońkowski T.

• Warsaw University of Technology, Warsaw, Poland

autor

Kłysz S.

• University of Warmia and Mazury, Olsztyn Air Force Institute of Technology, Warsaw, Poland

Bibliografia

• [1] Aerospace Systems Survivability Handbook Series. Volume 5. Survivability Models and Simulations, JTCG/AS-01-D-007, Joint Technical Coordinating Group on Aircraft Survivability (JTCG/AS), Arlington VA,31 July 2001.
• [2] Ball, R.E. (2003). The Fundamentals of Aircraft Combat Survivability Analysis and Design. AIAA.
• [3] Bedford, T. & Cooke, R. (2001). Probabilistic Risk Analysis: Foundations and Methods. Cambridge University Press.
• [4] Couch, M. & Lindell, D. (2010). Study on Rotorcraft Survivability, Aircraft Survivability: Rotorcraft Survivability, 9-13, 30.
• [5] Dotseth, W.D. (1971). Survivability Design Guide For U. S. Army Aircraft. Volume I. Small-Arms Ballistic Protection. USAAMRDL Technical Report 71-41A.
• [6] Failure Mode, Effects and Criticality Analysis (FMECA), CRTA-FMECA, Reliability Analysis Center, 1993.
• [7] Gary, L. Guzie (2000). Vulnerability Risk Assessment, ARL-TR-1045, Army Research Laboratory.
• [8] Jerome, C.L. (2011). Fixed-Wing Aircraft Combat Survivability Analysis For Operation Enduring Freedom And Operation Iraqi Freedom, AFIT/GAE/ENY/11-M14, Air Force Institute Of Technology.
• [9] MIL-STD-1629A, Procedures for performing a failure mode, effects and criticality analysis, Department of Defence United States of America, 24 November 1980.
• [10] MIL-HDBK-336-1, Survivability, Aircraft, Nonnuclear, General Criteria – Volume 1, Department of Defence United States of America, 25 October 1982.
• [11] Sprawozdanie Nr 113/31/2011. Analiza postaci i skutków uszkodzeń w warunkach bojowych (DMEA) zespołów i instalacji samolotu PZL-130 orlik TC II w oparciu o wymagania normy MILSTD-1629A, Instytut Techniczny Wojsk Lotniczych.