INTEGRATED AERODYNAMIC FIN AND STOWABLE TVC VANE SYSTEM
Assignee
US Government
Filed as: UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Filed
Mar 15, 1991
Granted
Jun 14, 1994
Location
INYOKERN CA US
Abstract
An aerodynamic fin and stowable jet vane system preferably for rocket motorissile applications to control roll, pitch, and yaw, in either the aerodynamic or thrust flight control conditions, has a retractable and stowable aerodynamic vane integrated with a stowable thrust vector reaction steering system on a common support. The integrated aerodynamic fins and thrust vector control reduce the overall missile mainframe dimensions and are mounted on a single, space saving support.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jun 19, 1991
Rescinded
Nov 30, 1993
Duration
2 years, 5 months
Inventor
- 1ARNOLD O. DANIELSON
Record Details
- Patent number
- US 5320304
- Application
- 07666104
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
US GovernmentMore from this assignee
PENTAFLUOROSULFANYLNITRAMIDE SALTS
US Government
TITANIUM ALLOY CONTAINING AL,V,MO,FE, AND OXYGEN FOR PLATE APPLICATIONS
US Government
HYDROGEN GENERATION APPARATUS FOR AN UNDERWATER VEHICLE
US Government
CONFORMING TUNING COUPLER FOR FLEXTENSIONAL TRANSDUCERS
US Government
CLOSED BRAYTON CYCLE DIRECT CONTACT REACTOR/STORAGE TANK WITH CHEMICAL SCRUBBER
US Government
CLOSED CYCLE BRAYTON PROPULSION SYSTEM WITH DIRECT HEAT TRANSFER
US Government
Related by domain
NEURAL NETWORK CONTROLLER FOR A PULSED ROCKET MOTOR TACTICAL MISSILE SYSTEM
Raytheon
MISSILE JET VANE CONTROL SYSTEM AND METHOD
HUGHES MISSILE SYSTEMS COMPANY
AIRCRAFT INFRARED GUIDED DEFENSE MISSILE SYSTEM
HEAT RADIATION DETECTION SYSTEM
GENERAL DYNAMICS
PASSIVE RANGEFINDER
SECRETARY OF STATE OF DEFENSE IN HER BRITANNIC MAJESTY'S GOVERNMENT OF THE UNITED KINGDOM OF GREAT BRITAIN AND NORTHERN IRELAND, THE
ANTITANK WEAPON FOR COMBATING A TANK FROM THE TOP
RHEINMETALL GMBH