An escape system extraction rocket proposed for use on the Rotor Systems Research Aircraft was tested at Mach numbers of 0.1 and 0.3 through an angle of attack range from -2 deg to 102 deg and an angle of sideslip range from 0 deg to 15 deg in the Langley 7- by 10-foot high speed tunnel.
Longitudinal and Lateral-Directional Static Aerodynamic Characteristics of an Unpowered Escape System Extraction Rocket Model
1977
26 pages
Report
No indication
English