Abstract: An improved method that directly and continuously determines the magnitude f the earth's gravity in relation to a user platform at one or more selected points on or above the earth's surface. An improved Global Positioning System (GPS) is used to carry out the method and is made up of a plurality of twenty-four (24) continuously orbiting GPS satellites that are arranged into three groups of eight satellites with each group or constellation being disposed in its respective plane of a series of three longitudinal planes. Each plane is arranged in predetermined angular and spatial relation to the earth's equatorial plane and the other planes of the series. Any GPS satellite continuously transmits a pair of encoded RF signals at predetermined L-band frequencies. By virtue of this global arrangement of the 24 satellites, the antenna field of view of a user platform is capable of receiving at any time the encoded signals of at least six satellites.
Type:
Grant
Filed:
February 27, 1984
Date of Patent:
November 5, 1985
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: 2-(4-pyridyl)-5-aryloxazoles and certain quaternary salts of these compounds are useful as visible-wavelength lasing dyes. These dyes are used in solution with non-interferring polar solvents, such as low molecular weight alcohols, H.sub.2 O, and D.sub.2 O, to form lasing media useful in dye lasers. Such lasers generally include a reservoir for containing the laser dye solution and a pumping energy source operably coupled therewith for producing stimulated emission of the dye solution.
Type:
Grant
Filed:
June 2, 1980
Date of Patent:
March 19, 1985
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: A monolithic multi-point initiator for a warhead wherein a single detonator s connected by multiple interconnected conduits packed monolithically with an initiator compound that delivers detonating waves to a series of multi-point explosive charges or pellets located at or near either end of the warhead.
Type:
Grant
Filed:
June 17, 1981
Date of Patent:
October 9, 1984
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: A rain erosion resistant protective covering for aircraft having pointed or conical radomes and method of forming the protective covering. The protective covering is a layered material of polyurethane, contact adhesive, and polyethylene which is formed into the desired shape by precutting the material to the shape of the radome, placing the material in a mold, heating the material, and drawing a vacuum between the mold and material to draw the material into the shape of the mold, thus producing a cover having the shape of the mold.
Type:
Grant
Filed:
September 21, 1981
Date of Patent:
March 13, 1984
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: Apparatus for stabilizing a weapon launched from an aircraft. The weapon is rovided with a plurality of concentric rings mounted on the nose of the weapon for reducing nose lift. The tail of the weapon is provided with a plurality of wedge shaped fins positioned on a decreasing tail diameter which increases the tail stability while minimizing tail lift. The outer faces of the fins are of a multi-tiered construction with angled portions connecting the tiers.
Type:
Grant
Filed:
September 21, 1981
Date of Patent:
January 24, 1984
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: The inclusion in a double base propellant of a ballistic modifier selected rom the class consisting of copper, lead, tin, and bismuth chelates of a dihydroxybenzophenone or alkoxyhydroxyphenzophenone.
Type:
Grant
Filed:
June 2, 1980
Date of Patent:
December 13, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: An apparatus for and a method of determining the material properties of a dielectric and/or conducting radar target by deciphering the backscattered signals returned from the target is disclosed. The resonance "code" of the echo signals from the target is a function of the width and spacing of the resonant spectral lines in the transverse electric (TE) and transverse magnetic (TM) modes of the returned signals. The resonances present in any TE or TM mode become uniformly spaced and of uniform width at high frequencies. The uniform spacing between adjacent resonances is used to uniquely determine the dielectric constant of the material comprising the target, and their uniform width is used to uniquely determine its thickness.
Type:
Grant
Filed:
June 26, 1981
Date of Patent:
November 15, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: A digitally activated display scale in association with digital-electronic ircuitry, displays both the airspeed and airspeed trend of a landing aircraft. The digital/electronic circuitry process an analog voltage corresponding to an airspeed range of 80 to 179 knots to produce a digital number representative of the airspeed of the landing aircraft. The digital number is used to produce a continuous display of the airspeed and to indicate the trend of the airspeed as either increasing or decreasing.
Type:
Grant
Filed:
June 11, 1981
Date of Patent:
November 15, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Inventors:
Owen B. Laug, Charles C. Gordon, Robert O. Stone
Abstract: A digital m of n correlation device using signal and reference shaft registers, modulo 2 adders, unique 1-bit D/A converters, and single resistor analog summing provides a very fast correlation product for pulse compression modulations such as phase or frequency shift keying. The compression ratio for the digital m of n correlation device, according to the present invention, is 168:1 (equal to the number of bits). The device is capable of bit rates in excess of 100 Mbps and is well suited for LSI fabrication.
Type:
Grant
Filed:
June 1, 1981
Date of Patent:
November 8, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: Uniquely integrating a search mirror and a deflection mirror with a passive ptical rangefinder and a remote sextant, enhances the operation of both devices. The improved rangefinder/sextant provides day/night 360.degree. azimuthal and at least -5.degree. to about 60.degree. elevational search capability with the additional capability of pointing the search mirror at a navigational star in a direction different from that of an imaging camera. Thus, the imaging camera, can be pointed at the sea horizon that is least obscured by haze and/or sea clutter, thereby allowing altitude readings under adverse conditions.
Type:
Grant
Filed:
June 25, 1981
Date of Patent:
November 8, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: N,N,N',N'-tetrakis(2-fluoro-2,2-dinitroethyl) oxamide, ##STR1## which is prepared by the following reaction sequence ##STR2## N,N,N',N'-tetrakis(2-fluoro-2,2-dinitroethyl) oxamide is a high density, energetic explosive which is melt castable as well as thermally and hydrolytically stable.
Type:
Grant
Filed:
December 21, 1981
Date of Patent:
November 8, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Inventors:
Michael E. Sitzmann, William H. Gilligan
Abstract: Unsymmetrical carbonates of the formula ##STR1## are prepared by the following reaction sequence ##STR2## where R and R' can each be --CH.sub.2 C(NO.sub.2).sub.3, CH.sub.2 CF(NO..2).sub.2, --CH.sub.2 CF.sub.2 (NO.sub.2), --CH.sub.2 CCl(NO.sub.2).sub.2, --CH.sub.2 CF.sub.3, --CH.sub.2 CCl.sub.3, --CH.sub.2 C(NO.sub.2).sub.2 CH.sub.3, or --CH.sub.2 CF.sub.2 CF.sub.2 H, provided that R.noteq.R' and wherein R" is a lower alkyl group of from 1 to 6 carbon atoms.Also included are symmetrical 1,3-bis(halo- and nitroalkyl carbonyldioxy)-2,2-dinitropropanes of the formula ##STR3## which are synthesis by the following reaction sequence ##STR4## wherein R and R" are as defined above. The carbonates of this invention are useful as energetic additives to propellants and explosive.
Type:
Grant
Filed:
March 3, 1982
Date of Patent:
October 25, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: Unsymmetrical carbonates of the formula ##STR1## are prepared by the following reaction sequence ##STR2## where R and R' can each be --CH.sub.2 C(NO.sub.2).sub.3, CH.sub.2 CF(NO..2).sub.2, --CH.sub.2 CF.sub.2 (NO.sub.2), --CH.sub.2 CCl(NO.sub.2).sub.2, --CH.sub.2 CF.sub.3, --CH.sub.2 CCl.sub.3, --CH.sub.2 C(NO.sub.2).sub.2 CH.sub.3, or --CH.sub.2 CF.sub.2 CF.sub.2 H, provided that R.noteq.R' and wherein R" is a lower alkyl group of from 1 to 6 carbon atoms.Also included are symmetrical 1,3-bis(halo- and nitroalkyl carbonyldioxy)-2,2-dinitropropanes of the formula ##STR3## which are synthesis by the following reaction sequence ##STR4## wherein R and R" are as defined above. The carbonates of this invention are useful as energetic additives to propellants and explosive.
Type:
Grant
Filed:
March 3, 1982
Date of Patent:
October 25, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: The invention is a planar x-y translator for precision alignment of one p relative to another comprising a mounting plate holder, an adjustable cradle and a housing wherein the cradle is spring biased within the housing by multiple spring means at the top of the cradle and tension means at the base of the cradle.
Type:
Grant
Filed:
March 2, 1981
Date of Patent:
October 11, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: An underwater excavator comprising a modular non-metallic cofferdam wherein ater under pressure exits from a plurality of nozzles along at least one side of the base of the cofferdam and a fluid driven eductor driven by pressurized fluid evacuates the suspended solids raised by the pressurized fluid that flows through the nozzles, with a plurality of small barrier nozzles located along one or more horizontal conduits used to sink the cofferdam.
Type:
Grant
Filed:
April 2, 1981
Date of Patent:
October 11, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Inventors:
Harry S. Williams, Jan B. Yates, John J. Reidy, Ernest Faccini, Terry E. Hill, William K. Shafley
Abstract: A transportable calibration and storage device for use in calibrating radion dosimeters. The calibration device comprises a drum filled with a radiation attenuating material that may be solid, water, or water-extended solid. This material shields the radiation source that is retained in a safe position in the drum at all times. During the calibration cycle the radiation source may be moved to a low or high calibration position within the drum so as to allow calibration of the dosimeter with a known radiation intensity.
Type:
Grant
Filed:
April 17, 1981
Date of Patent:
September 27, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy
Abstract: A turbulence generator is provided on the forward end of a free flight ornce device to induce a turbulent boundary layer over the surface of the device. The turbulent layer generated is thicker than the normal boundary layer and helps reduce drag disparity between similar ordnance devices.
Type:
Grant
Filed:
February 20, 1981
Date of Patent:
September 20, 1983
Assignee:
The United States of America as represented by the Secretary of the Navy