In air to air engagements with mobile threat helicopters, the possession of a round of ammunition which could depart from a normal flight trajectory to engage a maneuvering enemy target would be of great value. Maneuvering projectiles launched from an automatic cannon would have the added benefit of putting a number of rounds on target in a short time. The FC&SCWSL has initiated the development of such a projectile. In the sections that follow results of analytical investigation of the explosive thruster concept, which is only one of several maneuvering techniques, are described. (Author)
Analysis of Small Caliber Maneuverable Projectile (SCMP) Concepts for Helicopter and Air Defense Applications
1982
15 pages
Report
No indication
English
Ammunition, Explosives, & Pyrotechnics , Antiaircraft Defense Systems , Fin stabilized ammunition , Aircraft ammunition , Guided projectiles , Guided weapons , Gunfire , Maneuverability , Ammunition components , Thrusters , Ramburners , Guidance , Detection , Tracking , Target acquisition , Aerodynamics , Aircraft guns , Small arms ammunition , Helicopters , Feasibility studies , Air defense , Aerial warfare , Lateral explosive thrusters , Titable noses , Small caliber projectiles
Trajectory Control of a Small Caliber Projectile Using Active Transpiration
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