Accession Number:

AD0749027

Title:

Angular Momentum and the Aircraft-Store Separation Problem

Descriptive Note:

Technical rept.

Corporate Author:

NAVAL WEAPONS LAB DAHLGREN VA

Personal Author(s):

Report Date:

1972-04-01

Pagination or Media Count:

13.0

Abstract:

The stability criterion of a missile containing an internal spinning fly wheel is derived and the effect of this fly wheel on the missiles launch disturbance is explained.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE