United States of America As Represented by the Administrator of Nasa

Other

Phillips Petroleum Company

The United States of America As Represented by the Administrator of the

Plasma Processes, LLC

Richard R Holmes

Timothy N McKechnie

Chris A Power

Frank R Zimmerman

William K Witherow

Robert L Kurtz

Robert M Saxelby

Christopher A Power

Ronald L Daniel, Jr

An optical image enhancement system provides improved image contrast in imaging of a target in high temperature surroundings such as a furnace. The optical system includes a source of vertically polarized light such as laser and a beam splitter for receiving the light and directing the light toward the target. A retardation plate is affixed to a target-facing surface of the beam splitter and a vertical polarizer is disposed along a common optical path with the beam splitter between the retardation plate and the target. A horizontal polarizer, disposed in the common optical path, receives light passing through a surface of the beam splitter opposed to the target-facing surface. An image detector is disposed at one end of the optical path. A band pass filter having a band pass filter characteristic matching the frequency of the vertically polarized light source is disposed in the path between the horizontal polarizer and the image detector. The use of circular polarization, together with cross polarizers, enables the reflected light to be passed to the detector while blocking thermal radiation.

Laser image contrast enhancement system

A coating with the ability to protect (1) the inside wall (i.e., lining) of a rocket engine combustion chamber and (2) parts of other apparatuses that utilize or are exposed to combustive or high-temperature environments. The novelty of this invention lies in the manner a protective coating is embedded into the lining.

Rocket combustion chamber coating

A high temperature and highly corrosive resistant structure and method of fabricating the structure. In one embodiment of the present invention, vacuum plasma spray or other materials deposition techniques are used to fabricate the structure on a removable support member in the form of a gradient or composite structure that sequentially consists of a 100% ceramic interior layer, a first transition layer of ceramic/refractory metal, a layer of 100% refractory metal, a second transition layer of ceramic/refractory metal, and an outer layer of 100% ceramic material. In a second embodiment, the ceramic/refractory metal/ceramic cartridge is formed without transition layers between the ceramic and metal layers. In another embodiment of the invention the structure is fabricated on a removable support member by depositing an outer layer of ceramic material on a refractory metal. No transition layers of ceramic material/refractory metals are used. In a further embodiment of the present invention, the structure is fabricated on a removable support member by vacuum plasma spraying only a refractory metal on the removable support member which has a layer of a corrosion/oxidation preventative coating thereon which has been applied to the support member by vacuum plasma spraying or other material deposition technique.

High temperature and highly corrosive resistant sample containment

A process for making a combustion chamber for a rocket engine wherein a copper alloy in particle form is injected into a stream of heated carrier gas in plasma form which is then projected onto the inner surface of a hollow metal jacket having the configuration of a rocket engine combustion chamber. The particles are in the plasma stream for a sufficient length of time to heat the particles to a temperature such that the particles will flatten and adhere to previously deposited particles but will not spatter or vaporize. After a layer is formed, cooling channels are cut in the layer, than the channels are filled with a temporary filler and another layer of particles is deposited.

Method of fabricating a rocket engine combustion chamber

An armor structure is provided by laminating multiple units consisting of one or more ply of unidirectionally oriented polyolefin film or fibers which are positioned so that the lines of orientation of adjacent units are at angles to each other. The armor structure can either be used alone or in combination with other armor materials. Bonding of the plies is achieved solely through the application of heat and pressure to the composite of positioned plies.

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Guntersville, AL, United States of America

Richard R Holmes