AIRCRAFT ROUGH LANDING CRITERIA ARGUMENTATION BASED ON FLIGHT DATA READOUTS FROM MSRP-A-02
Abstract
Article considers methods of formation and argumentation of rough landing criteria based on the on-board MSRP-A-02 recorder data with an example of IL-76TD with PS-90A-76 gas-turbine engines. The volume of reliable information development on aircraft in-flight parameters and its maximum load factors on landing with different degree of roughness has been defined. The results of load quantity simulation have been analyzed.
References
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Review
For citations:
Filippov V.P. AIRCRAFT ROUGH LANDING CRITERIA ARGUMENTATION BASED ON FLIGHT DATA READOUTS FROM MSRP-A-02. Civil Aviation High Technologies. 2015;(219):104-109. (In Russ.)
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