METHOD OF COMPENSATING THE AIRPLANE'S TURNING MOMENT IN LANDING WITH A BRAKE PARACHUTE IN A STRONG SIDE WIND,
Abstract
The object of the invention is a method for compensating the turning moment of an airplane on landing with a brake parachute under conditions of a strong side wind which has the distinguishing feature that for the purpose of assuring a safe run of the airplane one releases after the basic brake parachute one of two supplementary stabilizing parachutes, as depends on the direction of the side wind, located on the wings symmetrically at the greatest distance from the center of gravity of the airplane. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 20, 1965
- Accession Number
- AD0621777
Entities
People
- M. S. Aretskin
- Ya. A. Livshits
Organizations
- National Air and Space Intelligence Center