Rocket propelled payload with divert control system within nose cone
US9018572B2 · kind B2 · utility
2Cited by
31References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 6, 2012 |
| Grant date | Apr 28, 2015 |
| Priority date | — |
| Expiry date | Jul 6, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B10/663
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.