D-SEND Experimental Data
To acquire the airborne boom measurement technique.
To make sure the possibility of the low-sonic-boom design concept validation with a scaled model.
To prepare the D-SEND#2 flight test
(Test protcol and measurement system check)
To demonstrate both front and rear shock shaping design.
To acquire the low-boom sonic-boom signature measurement
To obtain the validation data for low-boom sonic-boom signature
To establish sonic-boom measurement technique
(airborne, on the ground).
To gather the data for sonic-boom evaluation.
To make sure the validity of the flight test in the D-SEND project.
To obtain the validation data for sonic-boom prediction method.
English page was released.
D-SEND Database was released.
Copyright 2012 Japan Aerospace Exploration Agency