A STUDY OF OPEN SEAT AIRCRAFT EMERGENCY ESCAPE SYSTEMS

A study of open seat aircraft emergency escape systems is presented. Special attention is directed toward thrust requirements necessary to achieve improved seat trajectories. A two-dimensional, three degrees-of-freedom mathematical model of a rocket-powered ejection seat trajectory, including means...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Wade, Wallace R, MacDonald, Hugh D , Jr, DeStefano, Leonard A, DeLeo, James M
Format:	Report
Sprache:	eng
Schlagworte:	AERODYNAMICS Aircraft ALTITUDE ANALOG COMPUTERS CATAPULTS COMPUTER PROGRAMMING CONFIGURATIONS DIGITAL COMPUTERS EJECTION SEATS LAUNCHING MATHEMATICAL MODELS NONLINEAR DIFFERENTIAL EQUATIONS PARACHUTE DESCENTS ROCKETS SAFETY STABILIZATION THRUST TRAJECTORIES VELOCITY VERNIER ROCKET ENGINES
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!