Title:
Final Report-- BAYONET Project
Author(s):
Pelley, R L [Aero/Thermodynamics Section of the Douglas Aircraft Company Missile & Space Systems Division];
Sporing, R W [Controls Section of the Douglas Aircraft Company Missile & Space Systems Division]
Publication Date:
1966 Aug 01
Document Number(s):
SC-CR-66-2000X; ALSNL199700001321
Originating Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
OpenNet Entry Date:
1999 Sep 28
OpenNet Modified Date:
1999 Sep 28
Description/Abstract:
Means of increasing life and providing roll control for the BAYONET vehicle were studied. The results indicated that the optimum BAYONET configuration should employ slats, plain flaps, T-tail, and a jet roll control system.