omniomni/omni-engineering huggingface dataset:
Olin Palladium Award. The Olin Palladium Award (formerly the Palladium Medal Award) was established by The Electrochemical Society (ECS) in 1950 and is presented every 2 years to recognize outstanding contributions to the fundamental understanding of all types of electrochemical and corrosion phenomena and processes. 

The award consists of a uniquely designed palladium medal bearing the medalist’s name. The design of the medal depicts Pallas Athene employing a shield, on which the seal of the Society is inscribed, to protect the metals represented by ancient symbols from the elements, earth, air, fire, and water. Recipients are also presented with a wall plaque, cash prize, Electrochemical Society Life membership, and a free meeting registration.

History 
The Palladium Medal Award was initially funded by the royalties derived from the sales of the Corrosion Handbook and a gift of palladium metal from the International Nickel Company. The original purpose of the medal was to encourage research and achievement in the study of the corrosion of metals and its control, or in theoretical electrochemistry upon which the understanding of corrosion is based. 

In 1971 the scope was modified, and in 1977 the name was changed to The Olin Palladium Award after a generous endowment from the Olin Company.

Recipients 

As listed by ECS:

 2019 Shimshon Gottesfeld
 2017 Philippe Marcus
 2015 Digby MacDonald
 2013 Ralph E. White
 2011 Koji Hashimoto
 2009 
 2007 Sergio Trasatti
 2005 Robert A. Rapp
 2003 Eliezer Gileadi
 2001 Norio Sato
 1999 John B. Goodenough
 1997 Royce W. Murray
 1995 Jerome Kruger
 1993 Jean-Michel Savéant
 1991 John S. Newman
 1989 Brian Evans Conway
 1987 Allen J. Bard
 1985 Martin Fleischmann
 1983 Morris Cohen
 1981 Izaak Kolthoff
 1979 Roger Parsons
 1977 Heinz Gerischer
 1975 Marcel Pourbaix
 1973 Veniamin Levich
 1971 Leo Brewer
 1969 Thomas P. Hoar
 1967 Paul Delahay
 1965 Norman Hackerman
 1961 Herbert H. Uhlig
 1959 Alexander Frumkin
 1957 Karl-Friedrich Bonhoeffer
 1955 Ulick Richardson Evans
 1953 Nathaniel H. Furman
 1951 Carl Wagner

See also

 List of chemistry awards

References

External links

Olin Palladium Award 

Chemistry awards
Awards established in 1951
Gemini Powered Parachutes. Gemini Powered Parachutes was an American aircraft manufacturer based in Culver, Indiana. The company specialized in the design and manufacture of powered parachutes in the form of ready-to-fly aircraft under the US FAR 103 Ultralight Vehicles rules and the European Fédération Aéronautique Internationale microlight category.

The company was founded by a former employee of Buckeye Industries. It seems to have been founded about 2002 and gone out of business in 2007.

Gemini produced a series of single-seat powered parachutes, including the Gemini Classic, Gemini Star, Gemini Ultra Star and Gemini Viper. There was also one two-seat trainer model, the Gemini Twin which had sold 60 aircraft by 2005.

Aircraft

References

External links
Company website archives on Archive.org

Defunct aircraft manufacturers of the United States
Ultralight aircraft
Homebuilt aircraft
Powered parachutes
MTR CSR Sifang EMU. MTR CSR Sifang EMU may refer to either of the either of MTR's rolling stock:

 MTR CSR Sifang EMU (XRL), a MTR high-speed train to run on the Guangzhou–Shenzhen–Hong Kong Express Rail Link
 MTR CSR Sifang EMU (Local), a future MTR rolling stock to run on Kwun Tong line, Tsuen Wan line, Island line and Tseung Kwan O line
Flail space model. The flail space model (FSM) is a model of how a car passenger moves in a vehicle that collides with a roadside feature such as a guardrail or a crash cushion. Its principal purpose is to assess the potential risk of harm to the hypothetical occupant as he or she impacts the interior of the passenger compartment and, ultimately, the efficacy of an experimental roadside feature undergoing full-scale vehicle crash testing.

The FSM eliminates the complexity and expense of using instrumented anthropometric dummies during the crash test experiments. Furthermore, while crash test dummies were developed to model collisions between vehicles, they are not accurate when used for the sorts of collision angles that occur when a vehicle collides with a roadside feature; by contrast, the FSM was designed for such collisions.

History 
The FSM is based on research performed at Southwest Research Institute in 1980 and published in 1981 in the paper entitled "Collision Risk Assessment Based on Occupant Flail-Space Model" by Jarvis D. Michie. The FSM (coined by Michie) was accepted by the highway community and published as a key part of the "Recommended Procedures for the Safety Evaluation of Highway Appurtenances" published in 1981 in National Cooperative Highway Research Program (NCHRP) Report 230. In 1993, the NCHRP Report was updated and presented as NCHRP Report 350; in this research effort performed by the Texas Transportation Research Institute, the FSM was reexamined and was unmodified in the new publication. In 2004, Douglas Gabauer further examined the efficacy of the FSM in his PhD thesis. The American Association of State Highway and Transportation Officials (AASHTO) retained the FSM as the method of assessing the risk of harm to vehicle occupants in the 2009 "Manual for Assessing Safety Hardware" that replaced NCHRP Report 350, stating that the FSM had "served its intended purpose well".

Details 
The FSM hypothesis divides the collision into two stages.  In stage one, the unrestrained occupant is propelled forward and sideways in the compartment space due to vehicle collision accelerations and then impacts one or more surfaces (including the steering wheel) with velocity "V". According to the model, the vehicle (instead of the occupant) is the object that is accelerating. The occupant experiences no injury-producing force prior to contact with the compartment surfaces.

In stage two, the occupant is assumed to remain in contact with the compartment surface and experiences the same accelerations as the vehicle for the rest of the collision.  The occupant may sustain injury at the end of stage one based on the velocity of impact with the compartment surfaces and due to vehicle accelerations during stage two.  The occupant impact velocity and acceleration are computed from the vehicle collision acceleration history and the compartment geometry.  Finally, the hypothetical occupant impact velocity and acceleration are then compared to threshold values of human tolerance to these forces.

References

Scientific models
Applied mathematics
Mathematical modeling
Transport safety
USCGC Mallow. The USCGC Mallow (WLB-396) was a  belonging to the United States Coast Guard launched on 9 December 1943 and commissioned on 6 June 1944.

Design
The s were constructed after the s. Mallow cost $926,926 to construct and had an overall length of . She had a beam of  and a draft of up to  at the time of construction, although this was increased to  in 1966. She initially had a displacement of ; this was increased to  in 1966. It was powered by one electric motor. This was connected up to two Westinghouse generators which were driven by two Cooper Bessemer GND-8 four-cycle diesel engines. She had a single screw.

The Iris-class buoy tenders had maximum sustained speeds of , although this diminished to around  in 1966. For economic and effective operation, they had to initially operate at , although this increased to  in 1966. The ships had a complement of six officers and seventy-four crew members in 1945; this decreased to two warrants, four officers, and forty-seven men in 1966. They were fitted with a SL1 radar system and QBE-3A sonar system in 1945. Their armament consisted of one 3"/50 caliber gun, two 20 mm/80 guns, two Mousetraps, two depth charge tracks, and four Y-guns in 1945; these were removed in 1966.

Career 

Upon being commissioned in June 1944, Mallow was assigned to the 12th Coast Guard District and homeported in San Francisco where she was used for ATON in the Pacific until the end of World War II. After the war, starting in September 1946, she was stationed in Astoria, Oregon. In February 1958, Mallow assisted  with towing  6 miles south of Swiftsure Bank. In February 1989, she assisted with recovering debris from the United Airlines Flight 811 crash off Hawaii.
The Mallow was scrapped at the head of the Wicomico River in Salisbury Maryland.

See also
 List of United States Coast Guard cutters

References

External links

Historic American Engineering Record in Hawaii
Iris-class seagoing buoy tenders
1944 ships
Ships built in Duluth, Minnesota
John Boyd (trade unionist). Sir John McFarlane Boyd   (8 October 1917 – 30 April 1989) was a Scottish trade unionist.

Born in Motherwell, Boyd attended the Glencairn Secondary School before taking an engineering apprenticeship.  He became active in the Amalgamated Engineering Union (AEU), working full-time as a union organiser from 1946., and joining the union's executive in 1953.  He was also prominent in the Confederation of Shipbuilding and Engineering Unions, serving as its president in 1964, and was first elected to the General Council of the Trades Union Congress (TUC) in 1967.  A member of the National Executive Committee of the Labour Party, he also served as the party's chairman in 1967.

Boyd stood for the presidency of the AEU in 1967, but he lost out to the left-winger Hugh Scanlon.  In 1975, Boyd was elected as General Secretary of the AEU, serving until 1982.  He was known as a right-winger in the union movement and for his loyalty to the Labour Party.  From 1978 to 1982, he was also on the council of Acas; once retired from his trade union posts, he took up directorships of companies including ICL and the British Steel Corporation, and was a governor of the BBC.

Boyd was active in the Salvation Army from his childhood, and he received the Order of the Founder in 1981.  He was made a Commander of the Order of the British Empire in 1974, and was knighted in 1979.

References

1917 births
1989 deaths
Chairs of the Labour Party (UK)
General secretaries of the Amalgamated Engineering Union
People from Motherwell
Scottish Salvationists
Scottish knights
Commanders of the Order of the British Empire
SourceMeter. SourceMeter is a source code analyzer tool, which can perform deep static program analysis of the source code of complex programs in C, C++, Java, Python, C#, and RPG (AS/400). FrontEndART has developed SourceMeter based on the Columbus technology researched and developed at the Department of Software Engineering of the University of Szeged.

Background
During the static analysis, an abstract semantic graph (ASG) is constructed from the language elements of the source code. This ASG is then processed by the different tools in the package to calculate product metrics like LLOC, NLE or NOA, identify duplicate code (copy-pasted code; clones), coding rule violations, etc.

SourceMeter can analyze source code conforming to Java 8 and earlier versions, C/C++, RPG III and RPG IV versions (including free-form), C# 6.0 and earlier versions and Python 2.7.8 and earlier versions. 
In the case of C/C++, SourceMeter supports the ISO/IEC 14882:2011 international standard extended with several new features from ISO/IEC 14882:2014, and C language defined by the ANSI/ISO 9899:1990, ISO/IEC 9899:1999 and ISO/IEC 9899:2011 standards. Besides the standard features, several GCC and Microsoft specific extensions are also supported.

Features
 Precise and deep static analysis, building full semantic graphs, containing semantic edges (calls, references), comments, etc.
 60+ source code metrics (complexity, coupling, cohesion, inheritance, etc.), on different levels (package, namespace, class, method, etc.)
 Type-2 duplications regarding syntax boundaries
 Code duplication metrics (stability, embeddedness, dispersion, etc.)
 Detecting inconsistent changes of duplications
 Checking coding rules (Differences between PMD rule violations and FaultHunter rule violations)
 Detecting security vulnerabilities based on data-flow (SQL injection, XSS, etc.)
 Checking metric-based rule violations
 Checking Android specific rule violations
 Detecting runtime exceptions by means of symbolic code execution, for Java only

SonarQube plug-in

SourceMeter plug-in for SonarQube platform is an extension of the open-source SonarQube platform for managing code quality. The plug-in executes SourceMeter from the SonarQube platform and uploads the source code analysis results of SourceMeter into the SonarQube database. The plug-in is open-source, and provides all the usual SonarQube code analysis results, extended with many additional metrics and issue detectors provided by the SourceMeter tool. The plug-in supports the C/C++, Java, C#, Python and RPG languages.

References

External links

Static program analysis tools
software testing tools
Harmening's High Flyers. Harmening's High Flyers was an American aircraft manufacturer founded by Mike Harmening. It was originally based in Genoa, Illinois and later in Big Stone City, South Dakota. The company specialized in the design and manufacture of powered parachutes in the form of kits for amateur construction and ready-to-fly aircraft in the US FAR 103 Ultralight Vehicles rules.

The company was founded in 1988 and seems to have gone out of business in 2008.

Harmening's produced a whole range of powered parachutes including the base model High Flyer, Standard, Deluxe, Premiere, Executive and the High Five, all variants of the same basic design.

Aircraft

References

External links
Company website archives on Archive.org

Defunct aircraft manufacturers of the United States
Ultralight aircraft
Homebuilt aircraft
Powered parachutes
Helite Skydancer. The Helite Skydancer is a French powered parachute that was designed and produced by La Mouette of Messigny-et-Vantoux under their Helite brand. Now out of production, when it was available the aircraft was supplied as a complete ready-to-fly-aircraft.

The aircraft is no longer advertised for sale by either La Mouette or Helite. In 2015 Helite was singularly a producer of air bag products.

Design and development
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The aircraft has a maximum gross weight of . It features a parachute-style wing, two-seats-in-tandem accommodation, tricycle landing gear and a single  Rotax 582 engine in pusher configuration.

The aircraft carriage is built from a combination of bolted aluminium and 4130 steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates spring rod suspension.

Specifications (Skydancer)

References

Helite Skydancer
2000s French sport aircraft
2000s French ultralight aircraft
Single-engined pusher aircraft
Powered parachutes
Juan J. de Pablo. Juan J. de Pablo (born December 9, 1962), a chemical engineer, is the executive dean of the New York University Tandon School of Engineering and the University’s inaugural executive vice president for global science and technology. He assumed those posts on October 1, 2024. Prior to that, he was Liew Family professor in the Pritzker School of Molecular Engineering at the University of Chicago and has served as senior scientist at Argonne National Laboratory. In 2018, he was appointed Vice President for National Laboratories at the University of Chicago, a title which later expanded to include Science Strategy, Innovation and Global Initiatives in 2020. In 2021, he became Executive Vice President for Science, Innovation, National Laboratories and Global Initiatives at the University of Chicago. He is known for his research on the thermophysical properties of soft materials and was the co-director of the NIST supported Center for Hierarchical Materials Design (CHIMaD). and director of the UW-Madison Materials Research Science and Engineering Center (MRSEC).
He was elected a member of the National Academy of Sciences in 2022.

Education
De Pablo earned a bachelor's degree in chemical engineering from Universidad Nacional Autónoma de México in 1985. After completing his Ph.D. in chemical engineering from the University of California, Berkeley in 1990 under the advisement of John Prausnitz. De Pablo conducted his postdoctoral research at the Swiss Federal Institute of Technology in Zurich, Switzerland.

Honors and awards 
He was elected a member of the National Academy of Engineering in 2016 for design of macromolecular products and processes via scientific computation. He is also a fellow of the American Academy of Arts and Sciences, the American Physical Society and an honorary member of the Mexican Academy of Sciences. He is recipient of the AIChE Charles M.A. Stine Award for outstanding contributions to the field of materials science and engineering, the DuPont Medal for excellence in nutrition and health science, and the American Physical Society 2018 Polymer Physics prize  He holds over 20 patents on multiple technologies.

References

External links
 Research Group Homepage
 Google Scholar Page

University of Chicago faculty
National Autonomous University of Mexico alumni
UC Berkeley College of Chemistry alumni
1962 births
Mexican chemical engineers
Living people
Members of the United States National Academy of Sciences
Recipients of the Presidential Early Career Award for Scientists and Engineers
Infinity Purple. The Infinity Purple is an American powered parachute that was designed and produced by Infinity Power Chutes of Bronson, Michigan. Now out of production, when it was available the aircraft was supplied as a complete ready-to-fly-aircraft.

The Purple was in production in the early 2000s and, while now discontinued, it led to the later Infinity Commander light-sport aircraft model.

Design and development
The Purple complies with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . The aircraft has a maximum gross weight of . It also qualified as a US FAR 103 Ultralight Vehicles trainer. It features an APCO Aviation parachute-style wing, two-seats-in-tandem accommodation, tricycle landing gear and a single  Rotax 582 engine in pusher configuration.

The aircraft carriage is built from welded 4130 steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. The throttle is a handle-type. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates spring rod suspension and off-road tires.

The aircraft has an empty weight of  and a gross weight of , giving a useful load of . With full fuel of  the payload for crew and baggage is .

Specifications (Purple)

References

Purple
2000s United States sport aircraft
2000s United States ultralight aircraft
Single-engined pusher aircraft
Powered parachutes
Gateway Galactic. Gateway Galactic, Inc. was formed in 2014 in Ames, Iowa and is an aerospace company with the goal to reduce the cost of commercial spaceflight, and is currently developing an orbital propellant depot, Antaios.  Gateway Galactic was founded by Justin Myers and Floyd Richardson, who currently operate as the company's key executives.

Antaios
Antaios is a propellant depot currently in development by Gateway Galactic, Inc. The name Antaios is an indirect reference to Anti, the ferryman in ancient Egyptian mythology. Anti's role was to grant Horus passage between the human world and their world. Much like Anti, Antaios will allow passage to far away locations in a more cost effective way.

Gateway Galactic is pioneering the new industry of selling fuel in orbit. An innovative feature of Antaios is its space saving design allowing it to be small enough for a single launch, yet large enough to handle the vast quantities of fuel that will be needed.

Propellant offered 
 Rocket Grade Kerosene - RP1
 Liquid Hydrogen - LH2
 Liquid Methane - LCH4
 Liquid Oxygen - LOX

See also

 List of space stations
 Private spaceflight
 Propellant depot
 Space colonization

External links
 
 Antaios 

Companies based in Iowa
Proposed space stations
Private spaceflight companies
Aerospace companies of the United States
De Marçay Passe-Partout. The de Marçay Passe-Partout (; ) was a small, low-powered single-seat sport and touring aircraft built in France just after World War I.

Design and development

The Passe-Partout was the smallest and lightest de Marçay aircraft of the three on display at the Paris Aero Salon of 1919. It had a very low power engine, the same  ABC 8 hp adapted flat-twin motorcycle engine that powered the English Electric Wren.  Flight magazine doubted its practicality with this engine.

It was a single bay biplane with a single interplane strut on each side defining a bay braced with a single flying wire and a single landing wire. Both wings  were two spar structures; there was marked forward stagger but no dihedral The interplane struts were slender at the top but smoothly widened towards their feet, linking the upper rear spar to both lower wing spars. The narrow upper joint provided a fixed point about which control wires could warp the trailing edge. Short cabane struts from the fuselage supported the centre of the upper wing. 

The Passe-Partout had a monocoque fuselage of rounded rectangular cross-section.  Its engine was mounted, with cylinders exposed, in the upper nose. The pilot's open cockpit placed him just aft of the upper trailing edge but over the lower wing because of the stagger.  At the rear a plywood covered tailplane was mounted high on the fuselage and fitted with fabric covered elevators. Both the fin and rounded rudder were also ply covered. Its  fixed landing gear was of the conventional tailskid type with mainwheels on a single axle rubber rubber sprung from a frame consisting of two V-form struts from the lower fuselage with a single cross-member.

The Passe-Partout hadn't yet flown when it appeared at the Paris Salon in December 1919 but it had flown by the following May. Marçay continued to advertise it until at least October 1920 but Flight's doubts about its practicality seem to have been justified for in May 1928, when the de Marçay company ceased to exist, Les Ailes noted that the Passe-Partout had undertaken only a few, inconclusive trials and further, that de Marçay himself saw it more of a curiosity than a practical aircraft.

Specifications

References

Citations

Bibliography

1920s French sport aircraft
Passe-Partout
Single-engined tractor aircraft
Biplanes
Aircraft first flown in 1920
Infinity Power Chutes. Infinity Power Chutes, LLC is an American aircraft manufacturer currently based in Uniondale, Indiana and headed by Frank Williams since 2019. It was originally located in Bronson, Michigan then moved to Sturgis, Michigan. The company specializes in the design and manufacture of powered parachutes in the form of ready-to-fly aircraft under the US FAR 103 Ultralight Vehicles rules, the European Fédération Aéronautique Internationale microlight and the American light-sport aircraft categories.

Infinity is a limited liability company.

The company currently offers two models of powered parachute, the Infinity Commander two seat light sport aircraft and the Infinity Challenger single-seater. The US Federal Aviation Administration had 191 aircraft made by Infinity registered in July 2015.

Aircraft

References

External links

Aircraft manufacturers of the United States
Ultralight aircraft
Powered parachutes