Aircraft LASTA take-off and landing performance

Abstract

Analysis of the take-off and landing distance of a single tractor propelled aircraft LASTA is presented in this paper. The purpose of the analysis is to enable certification of the LASTA aircraft according to civil regulations CS-23. The paper presents the approximated method for calculating take-off and landing distance and compares it with the flight test results. Good agreement between these two results is obtained.

Keywords

• take-off performance
• landing performance
• single-engine aircraft
• flight tests