ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE

A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.

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Bibliographic Details
Main Authors ALKEMA, MICHAEL S, FACCIANO, ANDREW B, MOORE, ROBERT T
Format Patent
LanguageEnglish
French
German
Published 27.07.2016
Subjects
AMMUNITION
BLASTING
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.
Bibliography:Application Number: EP20130853167