Abstract: A pulsed transformer having a superconducting primary winding and a normal conducting secondary winding. The secondary winding is connected across a load. One side of the secondary winding has a switch in series to the load. A high energy storage inductor is connected in parallel across the switch. With the switch closed and the primary winding and storage inductor charged to their maximum capacity, a high level of current now flows through the switch. The primary is then caused to go into its normal conducting mode collapsing the primary field which induces current into the secondary winding. As the secondary winding current increases the high level of current normally flowing through the switch decreases to substantially zero. When the switch current reaches substantially zero, the switch can be opened without damage thereto releasing the high energy from the storage inductor into the load. The switch primary winding can be constructed from a high temperature superconductor for improved performance.

Abstract: A fastener for connecting structures having significantly different coefficients of thermal expansion which substantially eliminates thermal stress with varying ambient temperatures, while allowing said structures to be offset or spaced from each other. A frusto-conical bore through a wall of a first structure receives a frusto-conical surface of an elongated fastener which is coincident with said bore. The fastener has a base secured to a second structure. A shoulder is formed on said first structure around the narrow end of said bore, the shoulder having a frusto-conical outer edge. A flange member is secured to the vertex end of said fastener, said flange member having a surface configured to engage said outer edge in a coincident relationship. The fastener is tightened to bring both pairs of coincident conical surfaces into pressure contact. Both pairs of conic surface preferably have a common vertex which lies outside the fastener.

Abstract: The disclosure is directed to a system for recovery of liquid fuel rocket engines used in space flight. The system comprises a sphere with a normally circumferential open portion for containing a rocket engine. The sphere is fixedly attached to the space vehicle. The engine is attached to the inner surface of the sphere in a manner allowing normal engine functions including but not limited to gimbaling. The normal engine hookup is provided via disconnects on the outer surface of the sphere. A pair of sphere closure sections are carried on rails within the sphere adjacent to the normally open portion of the sphere. When the use of the engine in space flight is completed generally prior to vehicle orbit, actuation devices translate the closure sections into the normally open portion of the sphere sealing the opening thereby forming an integral closed sphere, the sphere containing the engine is disconnected from the vehicle by explosive bolts or the like and then the sphere falls from the vehicle towards earth.

Abstract: A joint assembly for holding electrical conductors together comprises a connector which loosely engages the conductors when the assembly is subjected to relatively high temperatures. The connector is made of a material which has a sufficiently higher coefficient of expansion then the coefficient of expansion the material used for the electrical conductors in order to cause a differential shrinkage of the connector onto the conductors for a clamping engagement therebetween when the assembly is subjected to relatively low temperatures.

Abstract: A thermostat (10) comprising a metal hydride (26) encased in a bellows (16) and a second bellows (20) encasing available hydrogen gas (32) to be adsorped and desorped by the metal hydride (26). The metal hydride (26) mechanically expands its encasing bellows (16) during adsorption and contracts during desorption of the hydrogen gas while a change in gas pressure due to this adsorption/desorption expands and contracts its encasing bellows (20). Each bellows (16,20) is oppositely acting and each engage a valve seat (36,40), respectively, so that the flow of fluid is directed alternately through one valve seat opening or the other depending upon temperature affecting the gas absorping/desorping properties of the metallic hydride. The temperature at which the thermostat (10) operates may be adjusted by controlling the pressure of the gas in the gas bellows. Also disclosed is a variation of the invention as a thermal switch for space applications.

Abstract: A space rail (10) having two basic elements, a box structure (12) which is configured to permit installation of payload hardware and payload services hardware along its length and a deployable back structure (14) which provides stiffness to the assembly of space rails when deployed. The box structure (10) is preferably a flat rectangular frame comprising body members (12) and the back structure (14) comprises a plurality of struts (24a-d, 30) pivotally attached to the body member (14) and to each other so as to fold into a retracted deployable position and to be deployed (unfolded) by a suitable mechanism.

Abstract: Metallic insulation for superconducting magnets to provide coil to coil and pancake insulation. Exemplary metal alloys and an anodization coating for such insulation are identified and may be selectively removed to provide shunt current paths. The coating for such insulation may be selectively removed to provide shunt current paths when the coil experiences a quench condition to preclude coil damage. Various applications of metallic insulation to superconducting coils are discussed.

Abstract: Disclosed is a method of placing a measured amount of tracer material into a release agent solution so that the concentration of tracer material in the release agent as applied to a mold surface is an indication of the amount and distribution of the release agent on the mold surface. The release agent can be applied and/or re-applied until the amount of the tracer material reaches a predetermined value. In the embodiment disclosed the tracer material is a UV dye which will re-emit light when activated by a UV light source and the intensity level of the re-emitted light is a function of the amount of release agent applied.Curing of the release agent preferrably taken place after each layer in multiple layer applications.Also disclosed is a spray head (12) connected to a source (20) of release agent with UV dye therein for coating a mold surface (28). A source of UV light (30,32) activates the UV dye to re-emit visable light which is measured by a photometer (34) to practice the above method.