Accession Number:

AD0370568

Title:

TEST DOLLY, VARIABLE ANGLE, FUEL SYSTEM DEVELOPMENT, TRANSPORTER,

Descriptive Note:

Corporate Author:

LOCKHEED AIRCRAFT CORP VAN NUYS CALIF

Personal Author(s):

Report Date:

1956-01-23

Pagination or Media Count:

14.0

Abstract:

This report describes the design, construction, and use of a dolly in development testing of the XQ-5 fuel system. The finished product is believed to be readily adaptable to accommodate future possible variations of the existing fuel system. Author

Subject Categories:

  • Pilotless Aircraft
  • Surface Transportation and Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE