Abstract: An automatic drainage system is described for draining one of two non-miscible liquids which are of different densities from at least one tank (1) via a drain valve (3,10,60) including a system for monitoring the relative proportions of the non-miscible liquids in the liquid flow along the drain line (2). According to the invention the monitoring system includes a recirculating path (2A, 26 FIGS. 1 to 5: 2A FIG. 6) for liquid from the drain line (2) back to the tank (1), a pump (5) in the recirculating path for moving liquid around the path, the pump being arranged to maintain a substantially constant liquid flow around the path substantially independently of the head of liquid in the tank, a detector (7) in the path having at least one sensing head (8) for sensing the relative proportions of the two non-misible liquids flowing in said path, and control means (9) for controlling the system in dependence upon said relative proportions.

Abstract: An offset collapsible/deployable dish having solid, relatively rigid folding panels which are unfoldable to a dish configuration conforming to an offset surface of revolution, such as an offset paraboloid generated about an axis offset from the dish, and foldable to a collapsed configuration contained within an envelope substantially smaller than the rim diameter of the dish. A radiation device utilizing the offset dish as a microwave, optical, or high energy beam reflector.

Abstract: An improved hydraulic reflector is provided for use as an antenna or solar reflector or the like, wherein the reflector is collapsible for highly compact stowage within a space vehicle and for convenient deployment in space to an expanded, generally dish-shaped configuration. The reflector comprises a rigid central dish hinged to a peripheral array of hingedly interconnected rigid panels which in turn carry a peripheral array of outwardly radiating extension ribs supporting an outer ring of flexible reflector material. The rigid panels and the extension ribs are movable together between a collapsed state folded substantially into a cylindrical envelope defined by the diametric size of the rigid central dish and a deployed configuration lying generally within a surface of revolution common to the central dish, such as a paraboloid surface in the case of an antenna.

Abstract: A releasable coupling assembly is provided for secure retention and controlled reliable release of a releasable structure with respect to a base structure, such as a releasable spacecraft with respect to a mother spacecraft or launch vehicle. The releasable coupling assembly comprises a latch housing on the base structure and supporting a pair of pivotal latches for locking engagement with oppositely projecting locking tabs of a pawl rotatably supported on a locking shaft mounted on the releasable structure. The two latches are respectively coupled to a pair of control pistons movably disposed within cylinders in the latching housing and biased by springs toward normal positions in locked engagement with the pawl. Supply of a fluid under pressure to the cylinders displaces the control pistons in directions retracting the latches to release positions disengaged from the pawl thereby releasing the locking shaft and the releasable structure from the base structure.

Abstract: A fluid coupling assembly is provided for fluid transfer with relatively small pressure loss between a pair of fluid flow conduits and with little or no fluid spillage upon subsequent conduit separation. The coupling assembly comprises male and female valve units mounted respectively on the flow conduits and matingly engageable to align valve unit flow paths for fluid transfer between the flow conduits. The flow path of each valve unit is normally closed by an externally finned, motor-driven poppet valve having a valve head contoured for seated reception onto a valve seat and for substantially flush surface abutting engagement with the valve head of the other poppet valve to define a substantially minimum residual volume between the valve heads when the two valve units are matingly engaged.

Abstract: A collapsible dish structure composed of a plurality of rows of rigid radial petal assemblies concentric with the axis of the dish. The petal assemblies consist of a center petal and two side petals, the center petal hinged on an axis tangent to a circle concentric with the axis of the dish and the side petals hinged to the center petal at their mating edge. The center petal is foldable inwardly and the side petals rotate about their hinges such that the collapsed dish structure occupies a much smaller volume than the deployed dish. Means of controlling the shape of the dish to compensate for differential expansion of the deployed dish are also provided.

Abstract: A nozzle employed as a burner within a fluidized bed is coaxially enclosed within a tubular shroud that extends beyond the nozzle length into the fluidized bed. The open-ended shroud portion beyond the nozzle end provides an antechamber for mixture and combustion of atomized fuel with an oxygen-containing gas. The arrangement provides improved combustion efficiency and excludes bed particles from the high-velocity, high-temperature portions of the flame to reduce particle attrition.