Accession Number:

AD0692518

Title:

AIRCRAFT INTERFEROMETER DEVELOPMENT.

Descriptive Note:

Final rept. 1 May 66-30 Nov 68,

Corporate Author:

IDEALAB INC FRANKLIN MASS

Personal Author(s):

Report Date:

1969-04-01

Pagination or Media Count:

34.0

Abstract:

In this report the special features of the three interferometers flown successfully in a KC-135 aircraft are discussed. The vibration disturbance in the aircraft required that the interferometer servo be made stiffer. The steps taken to accomplish this are presented. The special shaker table used to check the interferometer for its vibration sensitivity is described. Author

Subject Categories:

  • Transport Aircraft
  • Test Facilities, Equipment and Methods
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE