Accession Number:

AD0645998

Title:

INSTALLED SYSTEMS FUNCTIONAL TEST SUMMARY

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1964-03-01

Pagination or Media Count:

22.0

Abstract:

The the XV-5A aircraft SN 24506 was ground tested in all areas pertaining to hover, forward fan supported flight, and low speed conventional flight and is acceptable to proceed into active flight testing.

Descriptors:

• *RESEARCH AIRCRAFT
• *VERTICAL TAKEOFF AIRCRAFT
• AIRCRAFT ENGINES
• FLIGHT
• HOVERING
• LIFT
• PROPULSION SYSTEMS

Subject Categories:

• VSTOL
• Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE