Special Coverage

Supercomputer Cooling System Uses Refrigerant to Replace Water
Computer Chips Calculate and Store in an Integrated Unit
Electron-to-Photon Communication for Quantum Computing
Mechanoresponsive Healing Polymers
Variable Permeability Magnetometer Systems and Methods for Aerospace Applications
Evaluation Standard for Robotic Research
Small Robot Has Outstanding Vertical Agility
Smart Optical Material Characterization System and Method
Lightweight, Flexible Thermal Protection System for Fire Protection
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Supercomputer Cooling System Uses Refrigerant to Replace Water

Sandia National Laboratories researchers designed a cooling system for supercomputer centers that is expected to save four to five million gallons of water annually in New Mexico if installed at Sandia's computing center, and hundreds of millions of gallons nationally if the method is widely adopted. It is being tested at the National Renewable Energy Laboratory (NREL), which expects to save a million gallons annually. The system, built by Johnson Controls and called the Thermosyphon Cooler Hybrid System, cools like a refrigerator without the expense and energy needs of a compressor.

Posted in: Briefs, Electronics & Computers, Computer software and hardware, Product development, Cooling, Refrigerants

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Transformable and Reconfigurable Entry, Descent, and Landing Systems and Methods

This technology can be used in human and robotic space missions, and small satellite retrieval missions.NASA has developed a game-changing deployable aeroshell concept for entry, descent, and landing (EDL) of large science and exploration-class payloads. The Adaptable, Deployable Entry Placement Technology (ADEPT) concept is a mechanically deployable semi-rigid aeroshell entry system capable of achieving low ballistic coefficient during entry suitable for a variety of planetary or Earth return missions. It leverages Ames expertise in Thermal Protection Systems (TPS) material and entry system design, development, and testing. The deployable decelerator systems offer a lighter-weight solution to current rigid, high-ballistic-coefficient aeroshells. The deployable feature of ADEPT allows each mission to utilize an entry system design that fits within existing launch vehicle systems, and later transforms into a low ballistic coefficient configuration for EDL. Consisting of rigid ribs and a TPS, deployment can be done for inspection in Earth orbit by extending the ribs and stretching the TPS in between (in a method similar to an opening umbrella), and thereby reducing the mission risk.

Posted in: Briefs, Aeronautics, Aerospace, Aircraft structures, Entry, descent, and landing, Reusable launch vehicles and shuttles

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Three-Band Cloud and Precipitation Radar

After many years of use of Tropical Rainfall Measurement Mission (TRMM) and CloudSat data, focus groups within the cloud and precipitation science community produced requirements for the next generation of missions. The first draft of Aerosol-Cloud-Ecosystem mission requirements was formalized in 2009, snowfall observation requirements were documented in 2011, and recently the discussion for the definition of a mission concept called the Cloud and Precipitation Process Mission (CaPPM) has been initiated.

Posted in: Briefs, Green Design & Manufacturing, Architecture, Radar, Weather and climate

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High Speed Idle Engine Control Mode

Innovators at NASA's Glenn Research Center have developed an engine control mode that improves an engine's responsiveness to throttle commands during emergency landing conditions. The high speed idle (HSI) control mode increases the speed of the engine's fan and core shafts, allowing faster response and increased maneuverability during landing conditions when engines are in a low-power state. The innovation uses existing engine actuators to change the engine operating point to allow for faster engine response. Use of HSI increases fuel consumption, but it is anticipated to be used only in emergencies where the additional engine performance will help improve aircraft survivability.

Posted in: Briefs, Aeronautics, Aerospace, Sensors and actuators, Engine control systems, Hazards and emergency management, Hazards and emergency operations, Entry, descent, and landing

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Development of the Orion Crew-Service Module Umbilical Retention and Release Mechanism

The design is highly modular, and can easily be adapted to other vehicles/modules and alternate commodity sets.The Orion Crew-Service Module (CM/SM) umbilical retention and release mechanism supports, protects, and disconnects all of the cross-module commodities between the spacecraft's crew and service modules. These commodities include explosive transfer lines, wiring for power and data, and flexible hoses for ground purge and life support systems. Initial development testing of the mechanism's separation interface resulted in binding failures due to connector misalignments. Separation of the umbilical lines between the Crew Module (CM) and the Service Module (SM) happens as part of the vehicle separation activities prior to reentry. If the umbilical fails to separate successfully, the crew and spacecraft will likely be lost.

Posted in: Briefs, Mechanical Components, Mechanics, Architecture, Fasteners, Entry, descent, and landing, Spacecraft

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Blended Cutout Flap for the Reduction of Jet-Flap Interaction Noise

This technology preserves more of the aerodynamic load capacity of the wing flap, aileron, or flaperon.This technology is a new type of design for the wing flap, aileron, or flaperon located directly behind the engine nozzle on jet aircraft. Using a concave-down curved shape for the trailing edge instead of a conventional right angle, the cross section of the flap, aileron, or flaperon directly in the jet exhaust stream is reduced, thus reducing noise.

Posted in: Briefs, Aeronautics, Aerospace, Wings, Noise, Aerodynamics

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Computer Chips Calculate and Store in an Integrated Unit

Researchers at the University of Wisconsin-Madison created computer chips that can be configured to perform complex calculations and store massive amounts of information within the same integrated unit, and communicate efficiently with other chips. Called “liquid silicon” — liquid for software and silicon for hardware — the technology has uses in data-intensive applications such as facial or voice recognition, natural language processing, and graph analytics.

Posted in: Briefs, Electronics & Computers, Integrated circuits, Product development

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