omniomni/omni-engineering huggingface dataset:
Scheibe SF 40. The Scheibe SF 40 is a German two-seat ultralight aircraft designed and built by Scheibe Aircraft.

The SF 40 is a two-seat low-wing ultralight monoplane with a fixed tricycle landing gear. It has a fabric-covered steel-tube fuselage with fabric-covered glass-fibre wings. The first SF 40 powered by a Sauer four-stroke engine flew in 1995 but after five were built it was replaced in 1997 by an improved variant, the SF 40C. The SF 40C is powered by a Rotax 912 engine with a two-bladed propeller, a shorter wing span than the original with increased fuel capacity. The SF 40C was awarded a type certificate in May 1998.

Variants 
SF 40
Sauer-powered variant, five built.
SF 40C Allround
Rotax 912-powered variant.

Specifications (SF 40C)

References

Notes

Bibliography

 

1990s German civil utility aircraft
Motor gliders
Scheibe
Low-wing aircraft
Single-engined tractor aircraft
Aircraft first flown in 1995
Single-engined piston aircraft
Kelsey K-16. The Kelsey K-16 is an American, strut-braced, high-wing, two-seat, glider that was designed and constructed by William Frank Kelsey  of Salt Lake City, Utah.

Design and development
Kelsey completed the K-16 in 1961, and first flew in that year. The aircraft has a welded steel tube fuselage and a wooden structure wing, all covered in doped aircraft fabric covering. The  span wing employs a modified Göttingen airfoil. The landing gear is a center-line monowheel and a fixed skid.

Only one K-16 was built and it was registered with the US Federal Aviation Administration in the Experimental - Amateur-built and the Racing/exhibition categories.

Operational history
The aircraft was flown by its designer to earn his diamond badge goal flight. Kelsey subsequently sold it to the Soaring Society of Utah, who in turn sold it in the spring of 1971 to Robert J. Leonard of Soap Lake, Washington. In the autumn of 1972 the aircraft was severely damaged by a wind storm, with both wings damaged, including one that was broken into two sections. The aircraft was rebuilt as an Experimental Aircraft Association local chapter project. In August 2011, fifty years after the aircraft was built, Leonard was still listed on the FAA registry as the owner.

Specifications (K-16)

See also

References

1960s United States sailplanes
Homebuilt aircraft
Aircraft first flown in 1961
Lamson PL-1 Quark. The Lamson PL-1 Quark was an American high-wing, single-seat, glider that was designed and constructed by Philip Lamson, first flying in early 1965.

Design and development
Lamson designed and built the Quark in 1964 as a lighthearted experimental aircraft project to create a prone position-pilot glider. To this end the pilot was accommodated lying down with his head in the nose bubble.

The PL-1 is constructed from fiberglass, with the wings made from a balsa-fiberglass sandwich that was laid up in a female mold. The wing was originally of  span, but this was quickly increased to  with tip extensions and finally the aircraft received a new  three-piece wing. The airfoil was an Irv Culver modification to the NACA 0012. The landing gear was a monowheel, with small wing tip skids.

Soaring Magazine described the aircraft as "purely a lark and a quirky lark at that". The designer described the performance as "somewhere between a Nimbus and a Rogallo".

Only one Quark was built and it was registered with the US Federal Aviation Administration in the Experimental - amateur-built category.

Operational history
The aircraft logged about 300 hours in its  wingspan version. The Quark was removed from  the FAA registry on 13 August 2002 and the aircraft likely no longer exists.

Specifications (Quark)

See also

References

1960s United States sailplanes
Homebuilt aircraft
Prone pilot aircraft
Aircraft first flown in 1965
Brumby 600. The Brumby Aircraft Brumby 600, also known as the Brumby LSA 600 is an Australian single-engined, two-seat, training or touring cabin monoplane. The aircraft is built by Brumby Aircraft Australia as a production or kit aircraft at Cowra Airport near Cowra, New South Wales, Australia. Designed to meet regulations governing light sport aircraft (LSA), it was developed from the Goair Trainer.

Design and development
The Brumby was developed from the GoAir GT-1 Trainer, which was built at Bankstown Airport in Sydney during the late 1990s.

The Brumby 600 is a low-wing monoplane of all-metal construction. It has a fixed tricycle landing gear and an enclosed cockpit for two in side-by-side configuration with a forward-sliding canopy for access; sideways-opening gull-wing doors are available as an optional kit. It can be powered by a  Lycoming IO-233,  Rotax 912ULS or  Jabiru 3300 engine, driving a wooden two-blade propeller.

A high-wing version has been developed as the Brumby 610 Evolution.

Specifications

References

 
 

2000s Australian civil utility aircraft
Brumby Aircraft Australia aircraft
Low-wing aircraft
Single-engined tractor aircraft
Aircraft with fixed tricycle landing gear
Single-engined piston aircraft
Jain Institute of Technology. In the academic year 2011–2012, a new engineering college was started in Davangere called Jain Institute of Technology. It is affiliated to Visvesvaraya Technological University and approved by the All India Council for Technical Education.

Disciplines
The college provides four years full-time Bachelor of Engineering (B.E) degrees in the following streams:

 Civil Engineering
 Mechanical Engineering  
 Electronics Engineering 
 Computer Science Engineering 
 Electrical Engineering

PG programmes
M.B.A.

Besides B.E programs, the college also provides a two-year full-time Master of Business Administration.

References

Jain universities and colleges
Engineering colleges in Karnataka
Universities and colleges in Davanagere district
Education in Davangere
Educational institutions established in 2011
2011 establishments in Karnataka
Rhys Probert. Rhys Probert, CB (28 May 1921 – 1980), was a British aeronautical engineer. He was the son of the Reverend Thomas and Margaret Jane Probert of Blackwood, South Wales.

Early life
Probert had his first education at Jones West Monmouth School, then at St Catharine's College, Cambridge.

Career
From 1942-1944, Probert worked at the Royal Aircraft Establishment. He moved to Power Jets (Research and Development) Ltd in 1944, staying until 1946. He spent a brief time at the Applied Physics Laboratory, Johns Hopkins University, from 1946-1947. He joined the National Gas Turbine Establishment in 1947 and remained there until 1963 (as Deputy Director after 1957). Between 1963 and 1968, he was the Director-General of Scientific Research/Air, Ministry of Aviation. From 1968 until 1972, he was Deputy Controller of Aircraft, at the Ministry of Technology, and later the Ministry of Defence. Probert ended his career by returning to the Royal Aircraft Establishment as Director from 1973 until 1980. He was President of the Royal Aeronautical Society from 1979 until 1980.

Probert made notable contributions to many aircraft technologies, including ramjets, scramjets, vertical takeoff for Harrier jump jets, and reheat (afterburners).

His papers are available at the University of Cambridge, at  the Churchill Archives Centre.

Personal life
In 1947, Probert married Carolyn Cleasby, of Lancaster, New Hampshire, USA. They had three sons and one daughter.

He was made a Companion of the Bath in 1972. He died of pancreatic cancer in 1980.

References

1921 births
1980 deaths
20th-century British engineers
Alumni of St Catharine's College, Cambridge
Companions of the Order of the Bath
Jet engine pioneers
Power Jets
Welsh aerospace engineers
Yeomiji Botanical Garden. Yeomiji Botanical Garden () is botanical garden in Jungmun Tourism Complex, Seogwipo, Jeju-do, South Korea.

Inaugurated on October 12, 1989, Yeomiji used to be managed by Seoul Metropolitan Government. It was purchased by Buguk Development in 2005.

 Indoor gardens (over 1,300 species): under a massive sunflower-shaped structure, a  greenhouse featuring six thematic gardens (aquatic, flower, mystery, cactus, jungle, tropical), and a seasonal display.
 Outdoor gardens (over 1,000 species): four cultural gardens (Korean, Japanese, French, Italian), and theme gardens (endangered species and native plants, Jeju native plants, hosta garden, Rhododendron garden, herb garden, bog garden, lawn garden, cycas, perennial border).

References 
 Yeomiji Botanical Garden

Tourist attractions in Jeju Province
Botanical gardens in South Korea
Geography of Jeju Province
Sustainable furniture design. Sustainable furniture design and sustainable interior design is the design of a habitable interior using furniture, finishes, and equipment while addressing the environmental impact of products and building materials used. By considering the life-cycle impact of each step, from raw material through the manufacturing process and through the product's end of life, sustainable choices can be made. Design considerations can include using recycled materials in the manufacturing process, reutilizing found furniture and using products that can be disassembled and recycled or reclaimed after their useful life. Another method of approach is working with local materials and vendors as a source for raw materials or products. Sustainable furniture design strives to create a closed-loop cycle in which materials and products are perpetually recycled so as to avoid disposal in landfills.

Principles 
The principles of sustainable interior design will allow designers to reduce negative effects on the environment and build for a more sustainable future. These principles include the following:
 Energy efficiency
 Low environmental impact
 Reduce waste
 Use of healthy materials
 Create healthy indoor environments

Certifications 
 CLIMATE NEUTRAL Certified
 Cradle to Cradle
 FSC (Forest Stewardship Council)
 FTC (Fair Trade Certified)
 GREENGUARD
 GRS (Global Recycling Standard)
 Global Organic Latex Standard
 Global Organic Textiles Standard
 GreenScreen
 ISO14001
 ISO9001
 Indoor Advantage
 LEVEL by BIFMA
 MADESAFE
 OEKO-TEX

References

Further reading
 McDonough, W. & Braungart M. (2002). Cradle to Cradle: Rethinking the way we make things. New York, NY: North Point Press

External links 
  MBDC Cradle to Cradle Products
  EPEA GmbH

Furniture-making
Industrial design
Furniture
Pratt & Whitney R-2180-A Twin Hornet. The Pratt & Whitney R-2180-A Twin Hornet was a radial engine developed in the United States by Pratt & Whitney. It had two rows of seven cylinders each.

Applications
 Douglas DC-4E
 North American XB-21
 Republic P-44 Rocket
 Stearman XA-21

Specifications (R-2180-A)

See also

References

External links
 Aerofiles Reciprocating Engines page
 https://web.archive.org/web/20160411162935/http://www.enginehistory.org/P%26W/R-2180/R-2180Index.pdf

1930s aircraft piston engines
Aircraft air-cooled radial piston engines
R-2180
Fujitsu Celsius. The Fujitsu Celsius is a line of laptop and workstation computers manufactured by Fujitsu. The brand name has also been used for graphic accelerators. 

The laptops have Intel Core vPro, i5, or i7 processors, while the workstations have one or two Intel Xeon processors.

History and usage 
The computers are intended for applications such as computer-aided design, digital content creation, geographical information systems work, architecture, engineering, financial forecasting, flux balance analysis, scientific simulation, electronic design, and virtual reality.

Fujitsu Celsius equipment was used to stitch together thousands of individual photographic images to create large-scale 360-degree panoramic images: an 80-gigapixel image of London was published in November 2010, stating: “using this excellent workstation allowed this record-breaking photo to be created a few weeks faster than would have been possible on any other available PC.” The 320-gigapixel photomosaic of London published in February 2013 was prepared on a Celsius R920 in three months' time.

Models

Desktops 
Celsius R630 specs

Celsius R920  - 2012's model; The R920 is able to accept up to 512 GB of RAM.

Laptops 
Celsius H710 and Celsius H910 - 2011's models.

TFTS, “Fujitsu Brings Out Pair Of New Laptops, The Celsius H710 And The Celsius H910 [Described As Workstation Laptops, Fujitsu's New Hardware Offers Variety Of Configurations And High Power]”, Steve Anderson, May 23, 2011

See also
 Fujitsu Primergy servers and Fujitsu Esprimo desktops
 Dell Precision
 Lenovo ThinkStation
 Mac Pro
 HP Z

References

Mobile workstations
Fujitsu computers
Fujitsu laptops
Computer-related introductions in 1999
Leffler-MacFarlane LM-1. The Leffler-MacFarlane LM-1 is an American mid-wing, single-seat, FAI Open Class glider that was designed and constructed by Al Leffler, Walt MacFarlane and Bill Meyer, first flying in November 1963.

Design and development
The LM-1 was built using a modified wing from a Laister-Kauffman TG-4. The wing retains its original wood and doped aircraft fabric construction, its  span as well as the use of a NACA 4418 airfoil at the wing root, transitioning to a NACA 4409 at the wing tip. The newly designed fuselage is made from welded steel tube and fiberglass. The landing gear was originally a retractable dual-wheel hydraulic arrangement, that was replaced with a more conventional retractable monowheel from a Schreder HP-14.

The aircraft was registered with the US Federal Aviation Administration in the Experimental - Amateur-built category. Only one was ever constructed.

In 1974 it was reported that plans were underway to create a new  span wing for the LM-1, that would feature a Wortmann airfoil.

Operational history
By 1974 the LM-1 had flown  of cross country distance. In August 2011, 48 years after its first flight, the aircraft was still registered with the FAA and was owned by Bill Meyers, one of the original partners.

Specifications (LM-1)

See also

References

1960s United States sailplanes
Homebuilt aircraft
Aircraft first flown in 1963
The CIS Critical Security Controls for Effective Cyber Defense. The CIS Controls (formerly called the Center for Internet Security Critical Security Controls for Effective Cyber Defense) is a publication of best practice guidelines for computer security. The project was initiated early in 2008 in response to extreme data losses experienced by organizations in the US defense industrial base. The publication was initially developed by the SANS Institute and released as the "SANS Top 20." Ownership was then transferred to the Council on Cyber Security (CCS) in 2013, and then transferred to Center for Internet Security (CIS) in 2015. CIS released version 8 of the CIS Controls in 2021.

Goals
The guidelines consist of 18 (originally 20) key actions, called critical security controls (CSC), that organizations should implement to block or mitigate known attacks. The controls are designed so that primarily automated means can be used to implement, enforce and monitor them. The security controls give no-nonsense, actionable recommendations for cyber security, written in language that’s easily understood by IT personnel. Goals of the Consensus Audit Guidelines include

Leveraging cyber offense to inform cyber defense, focusing on high payoff areas
Ensuring that security investments are focused to counter highest threats
Maximizing the use of automation to enforce security controls, thereby negating human errors
Using consensus process to collect best ideas

Supported Platforms 
CIS Benchmarks cover a wide range of technologies, including:

 Operating Systems: Windows, Linux, macOS
 Servers: Apache, NGINX, Microsoft IIS
 Cloud Platforms: AWS, Azure, Google Cloud Platform
 Network Devices: Cisco, Juniper
 Applications: Microsoft Office, Google Chrome, Mozilla Firefox

References

Information privacy
Security compliance
Bernard SIMB V.1. The Bernard SIMB V.1 was a French single seat racing monoplane designed to compete for the 1924 Beaumont Cup.  It crashed on its first flight and was not rebuilt.

Design and development

The Bernard V.1 is alternatively known as the SIMB V.1: the Société Industrielle des Métaux et du Bois (SIMB) was the second of several aircraft companies founded successively by Adolphe Bernard.  The V.1 was a single-engine, single-seat monoplane designed to compete for the Beaumont Cup, a French competition held in 1924 requiring a 300 km (186 mi) flight round a 50 km (31 mi) circuit at Istres at an average speed of over 290 km/h (180 mph).

The V.1 had a cantilever shoulder wing of thin section, built around four spars with plywood and fabric covering.  Straight edged beyond the centre section, it tapered only slightly to the oblique tips. The tailplane had curved, swept leading edges and carried split elevators with a cut-out for rudder movement.  The fin was almost triangular, with a slightly convex leading edge; it carried a pointed rudder on a vertical hinge extending to the bottom of the fuselage.

The smooth, oval section fuselage was ply and fabric covered, tapering towards the tail.  The pilot sat low down in a small open cockpit with narrow streamlined dorsal fairings in front and behind.  His view forward was severely restricted by the central inline bank of four cylinders of the W-12 Lorraine-Dietrich 12E water-cooled piston engine. The engine was cooled by radiators in the wings, assisted for the first flight by a bank of radiators mounted between the undercarriage legs.  These backward leaning legs were wide chord, faired cantilevers with large, unfaired wheels mounted on individual stub axles.  The V.1's conventional undercarriage was completed by a small tailskid.

The racer was completed in nine months and taken to Istres in May 1924 to prepare for the competition.  Its first flight, piloted by Florentine Bonnet, ended in disaster. It was immediately apparent that the V.1 lacked longitudinal stability, oscillating uncontrollably in altitude; these oscillations persisted even as Bonnet reduced speed and attempted to land and the V.1 crashed at 200 km/h (125 mph), sliding on its back.  Bonnet was fortunate to escape unhurt.  The instability was ascribed to insufficient tailplane area combined with a far forward centre of gravity.  With the race only a few days away, there was no time to repair the V.1 and development was abandoned.

Specifications

References

Bibliography

V001
1920s French sport aircraft
Shoulder-wing aircraft
Single-engined tractor aircraft
Aircraft first flown in 1924
2014 in spaceflight. In 2014, the maiden flight of the Angara A5, Antares 120 and Antares 130 took place.

A total of 92 orbital launches were attempted in 2014, of which 88 were successful, two were partially successful and two were failures. The year also saw seven EVAs by ISS astronauts. The majority of the year's orbital launches were conducted by Russia, the United States and China, with 34, 23 and 16 launches respectively.

Overview
An Ariane 5 ES launched the Georges Lemaître Automated Transfer Vehicle, the last one of the series, which also marked 60 successfully completed Ariane 5 launches in a row.

On 22 August 2014, Arianespace launched the first two Full Operational Capability Galileo satellites for the European satellite navigation system.

A number of significant events in planetary exploration occurred in 2014, including the entry of the Rosetta spacecraft into orbit around the comet 67P/Churyumov–Gerasimenko in August 2014 and the deployment of the Philae lander to its surface in November, which marked the first orbit of and landing on a comet, respectively, and featured prominently in social media. Another notable occurrence was the entry of India's Mars Orbiter Mission into Martian orbit in September, making India the first Asian nation to reach Mars.

On 5 December 2014, a United Launch Alliance Delta IV Heavy launched the first Orion spacecraft test mission for NASA, Exploration Flight Test 1.

Orbital launches 

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Deep space rendezvous

Extra-Vehicular Activities (EVAs)

Orbital launch statistics

By country 
For the purposes of this section, the yearly tally of orbital launches by country assigns each flight to the country of origin of the rocket, not to the launch services provider or the spaceport. For example, Soyuz launches by Arianespace in Kourou are counted under Russia because Soyuz-2 is a Russian rocket.

By rocket

By family

By type

By configuration

By spaceport

By orbit

References

Footnotes 

 
Spaceflight by year
Imha Dam. The Imha Dam is an embankment dam on the Banbyeoncheon River, a tributary of the Nakdong River,  east of Andong in Gyeongsangbuk-do province, South Korea. The purpose of the dam is flood control, water supply and hydroelectric power generation. Construction on the dam began in 1987 and it was complete in 1991. The  tall rock-fill, central earth-core dam creates a reservoir with a capacity of  and supplies a 50 MW power station with water. It supplies water for both municipal and industrial uses to Gumi, Dagu, Masan, Changwon, Jinhae, Ulsan, and Busan.

See also

List of power stations in South Korea

References

Dams in South Korea
Hydroelectric power stations in South Korea
Rock-filled dams
Andong
Buildings and structures in North Gyeongsang Province
Dams completed in 1991
1991 establishments in South Korea
20th-century architecture in South Korea
PTC Creo. Creo is a family of Computer-aided design (CAD) apps supporting product design for discrete manufacturers developed by PTC.

Creo runs on Microsoft Windows and provides software for 3D CAD parametric feature solid modeling, 3D direct modeling, 2D orthographic views, Finite Element Analysis and simulation, schematic design, technical illustrations, and viewing and visualization. Creo can also be paired with the Mastercam machining based software.

History 
PTC began developing Creo in 2009, and announced it using the code name Project Lightning at PlanetPTC Live, in Las Vegas, in June 2010.

In October 2010, PTC unveiled the product name Creo. PTC released Creo 1.0 in June 2011.

Software and features 
Creo Parametric and Creo Elements compete directly with CATIA, Siemens NX/Solid Edge, and SolidWorks. The Creo suite of apps replace and supersede PTC’s products formerly known as Pro/ENGINEER, CoCreate, and ProductView.

See also 
 Autodesk Inventor
 Creo Elements/Pro
 Creo Elements/View
 I-DEAS
 Mastercam
 Parametric Technology Corporation
 Siemens NX
 Solid Edge
 SolidWorks

References

External links 
 

Product design
Computer-aided design software for Windows