Manufacturing & Prototyping

High-Pressure Lightweight Thrusters

Carbon/carbon composite structures are braided over iridium-lined mandrels and densified by chemical vapor infiltration. Returning samples of Martian soil and rock to Earth is of great interest to scientists. There were numerous studies to evaluate Mars Sample Return (MSR) mission architectures, technology needs, development plans, and requirements. The largest propulsion risk element of the MSR mission is the Mars Ascent Vehicle (MAV). Along with the baseline solid-propellant vehicle, liquid propellants have been considered. Similar requirements apply to other lander ascent engines and reaction control systems.

Posted in: Manufacturing & Prototyping, Briefs

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Robotic Exoskeleton Vastly Improves Quality of Life

Worldwide an estimated 185 million people use a wheelchair daily. A company based in Auckland, New Zealand, has developed an innovative robotic technology that helps people with mobility impairment get back on their feet— the Rex Bionics robotic exoskeleton. Its integrated maxon motors help to ensure smooth limb movement.

Posted in: Rehabilitation & Physical Therapy, Implants & Prosthetics, Biosensors, Mechanical Components, Power Supplies, Electronics, Power Management, Manufacturing & Prototyping, Motion Control, Motors & Drives, Power Transmission, Positioning Equipment, Medical, Orthopedics, Articles, Features, MDB

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Optimizing an Electromechanical Device with Multidimensional Analysis Software

Modern CAE software allows engineers to investigate a multitude of design variations that could not possibly be considered using conventional physical prototypes. In this paper we will first illustrate parametric methods for automatically creating virtual prototypes of electromechanical actuators (in our case simple electromagnetic solenoids) using the AMPERES and MAGNETO programs from INTEGRATED Engineering Software. We will then use a specific case study to show how the Tecplot Chorus program can assist in determining optimal design choices.

Posted in: Manufacturing & Prototyping, White Papers

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Ultrasonic Low-Friction Containment Plate for Thermal and Ultrasonic Stir Weld Processes

The thermal stir welding (TSW) process is finding applications in fabrication of space vehicles. In this process, workpieces to be joined by TSW are drawn, by heavy forces, between “containment plates,” past the TSW tool that then causes joining of the separate plates. It is believed that the TSW process would be significantly improved by reducing the draw force, and that this could be achieved by reducing the friction forces between the workpieces and containment plates.

Posted in: Manufacturing & Prototyping, Briefs

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High-Powered, Ultrasonically Assisted Thermal Stir Welding

This method has the potential to increase the longevity of hardware in the auto industry, especially in bearing wear. This method is a solid-state weld process capable of joining metallic alloys without melting. The weld workpieces to be joined by thermal stir welding (TSW) are drawn, by heavy forces, between containment plates past the TSW stir tool that then causes joining of the weld workpiece.

Posted in: Manufacturing & Prototyping, Briefs

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Next-Generation MKIII Lightweight HUT/Hatch Assembly

Applications for general aviation include the insulation around fuel tanks, especially winglocated tanks. The MK III (H-1) carbon-graphite/ epoxy Hard Upper Torso (HUT)/Hatch assembly was designed, fabricated, and tested in the early 1990s. The spacesuit represented an 8.3 psi (≈58 kPa) technology demonstrator model of a zero prebreathe suit. The basic torso shell, brief, and hip areas of the suit were composed of a carbon-graphite/epoxy composite lay-up. In its current configuration, the suit weighs approximately 120 lb (≈54 kg). However, since future planetary suits will be designed to operate at 0.26 bar (≈26 kPa), it was felt that the suit’s redesigned weight could be reduced to 79 lb (≈35 kg) with the incorporation of lightweight structural materials.

Posted in: Manufacturing & Prototyping, Briefs, TSP

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Additive Manufactured Propulsion System (AMPS) for Small to Micro Cubical Satellites

A hybrid, single-part design was fabricated from a material that acts as both the structure and the fuel for the propulsion system. The use of additive manufacturing technologies in aerospace applications has presented both opportunities and challenges. The ability to produce parts and components using additive manufacturing holds promise in both metals and plastics, whereas traditional subtractive manufacturing can be restrictive in design development and material selection.

Posted in: Manufacturing & Prototyping, Briefs

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