VARIABLE-THROAT CHIN INLET HIGH MACH NUMBER MISSILE APPLICATION
Assignee
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
Filed
Oct 19, 1981
Granted
Dec 1, 1992
Location
WETHERSFIELD CT US
Abstract
Variable chin-inlet for a missile wherein radially movable compression ramps vary the throat area so as to compress flow in the plane of the upstream boundary layer growth.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 13, 1982
Rescinded
Jul 20, 1992
Duration
10 years, 3 months
Inventor
- 1ARTHUR J. KARANIAN
Record Details
- Patent number
- US 5167249
- Application
- 06312605
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.More from this assignee
MODULATION FREQUENCY CONTROL IN A FIBER OPTIC ROTATION SENSOR
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
ROCKET NOZZLE FOR A ROCKET ENGINE
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
COOLABLE ROCKET NOZZLE FOR A ROCKET ENGINE
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
EXTERNAL WRAP OF COMPOSITE FLEXBEAM
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
RADIO FREQUENCY POWER MODIFICATION WITHOUT PHASE SHIFT
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
COLUMNAR GRAIN SUPERALLOY ARTICLES
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE.
Related by domain
IMPROVED PERFORMANCE EXLPOSIVE-FORMED PROJECTILE
GIAT INDUSTRIES
MULTIPLE INFRARED MISSILE JAMMER
LOCKHEED SANDERS INC, A DELAWARE CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
MISSILE LAUNCHER
MBM TECHNOLOGY LIMITED
AIR TO AIR HOMING MISSILE GUIDANCE
AIR FORCE, UNITED STATES OF AMERICA, AS REPRESENTED BY, THE SECRETARY
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION