Reaction Engines Limited
|Headquarters||Culham Science Centre, Oxfordshire, England|
|Products||Heat exchangers and propulsion systems for reusable space access and hypersonic flight|
History and personnel
Reaction Engines was founded in 1989 by Alan Bond (lead engineer on the British Interplanetary Society's Project Daedalus) and Richard Varvill and John Scott-Scott (the two principal Rolls-Royce engineers from the RB545 engine project). The company conducts research into space propulsion systems, centred on the development of the Skylon re-usable SSTO spaceplane. The three founders worked together on the HOTOL project, funding for which was withdrawn in 1988, largely due to significant technical obstacles.[clarification needed]
The division of responsibilities is:
- Mark Thomas CEng FRAeS, Managing Director (2015)
- Nigel McNair Scott, Non-Executive Chairman (2010)
- Tom Scrope, Finance Director (2014)
- Richard Varvill, Technical Director and Chief Designer
- Sam Hutchison, Director of Corporate Development (2012)
- Robert Bond, Corporate Programmes Director (2008)
- Gordon Harrison, Production Director (2010)
- John Garrod, as Non-Executive Director (1996)
In 2015 BAE Systems agreed to buy a 20% stake in the company for £20.6m as part of an agreement to help develop Reaction's Synergetic Air-Breathing Rocket Engine (SABRE) hypersonic engine designed to propel the Skylon orbiter.
Skylon and the SABRE engine by which it will be powered are being developed as a private venture which aims to overcome the obstacles that were imposed on further HOTOL development due to the British government classifying the HOTOL engine as an "Official Secret," and keeping the engine design classified for many years afterward.
The company's current research effort is focused on precooler heat exchanger technology, with additional funding gained from the sale of consultancy. The company has also received funding from the EU to investigate applications of its technologies to rapid long-distance passenger transport, under the LAPCAT project.
In February 2009, the European Space Agency announced that it was partially funding work on Skylon's engine to produce technology demonstrations by 2011. With this funding REL completed a non-frosting sub-zero heat exchanger demonstration program, Bristol University developed the STRICT expansion/deflection nozzle and DLR completed an oxidiser-cooled combustion chamber demonstration. REL claimed this work moved the Skylon project to a TRL of 4/5.
On 5 February 2008 the company announced it had designed a passenger plane to the concept stage. The A2 would be capable of flying, non stop, halfway around the world at hypersonic speed (Mach 5+).
The A2's engine, SCIMITAR, has precooler technology which is somewhat similar to SABRE, but does not have the rocket features, and is optimized for higher efficiency for atmospheric flight.
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In 2015 AFRL announced their analysis "confirmed the feasibility and potential performance of the SABRE engine cycle.” however they felt SSTO as a first application was a very high risk development path and proposed that a Two Stage to Orbit (TSTO) vehicle was a more realistic first step.
In 2016 AFRL released two TSTO concepts using SABRE in the first stage: The first 150 feet (46 m) long carrying an expendable upper stage in an underside opening cargo bay capable of delivering around 5,000 pounds (2.3 t) to a 100 nautical miles (190 km) orbit, the second 190 feet (58 m) long carrying a reusable spaceplane on its back, capable of delivering around 20,000 pounds (9.1 t) to a 100 nautical miles (190 km) orbit.
In March 2017, REL announced the formation of an American subsidiary, Reaction Engines Inc (REI), led by Adam Dissel in Castle Rock, Colorado.
In September 2017, REI announced a contract from DARPA to test a REL precooler test article "THX" at temperatures exceeding 1,000 °C (1,830 °F), previous precooler tests focusing on frost control having been conducted from ambient temperature.
Reaction Engines Ltd. is currently also researching more advanced spaceflight.
Passenger Module for Skylon
Although Skylon is designed to only launch and retrieve satellites, and that is also unmanned, Reaction Engines Ltd. has proposed a passenger module in the payload bay of the Reaction Engines Skylon spaceplane.
The passenger module is sized to fit in the payload bay, and can carry up to 24 passengers and 1 crew. There is an ISS-type docking port and airlock as the central feature. There are two ground entry doors that align with the doors on the side of the Skylon payload bay to allow easy ground access to the cabin. The doors are fitted with conventional inflatable chutes for passengers to escape in case of any ground emergency. There are Space Shuttle-type windows on the roof of the module for passengers to enjoy the view in space. There is also a washroom and hygienic facilities provided in the cabin.
The initial configuration will be fitted with five ejector seats, for four passengers and one crew, rather similar to the first four Space Shuttle spaceflights. Once the passenger module is fully certified, the ejection seats will be removed and there will be 16 upright seats installed for a short stay in space (<14 days) and 4 supine seats for long stay in space (>14 days). An upright seat will also be provided for the crew. There are also life support systems under the cabin floor, equipment bays, and cargo holds.
Orbital Base Station
The Orbital Base Station (OBS) is a concept of a future, expandable space station to serve as an integral part of a future space transportation system and also in the maintenance and construction of future manned Moon and Mars spacecraft.
The construction of the OBS is modular, and assumes the use of the Reaction Engines Skylon in Low Earth Orbit. The structure is based on a cylinder, designed to allow space inside the cylindrical section for the construction and repair of various spacecraft. The cylindrical structure will also provide space for habitation modules with docking ports, manipulator arms, and propellant farms to refuel an interplanetary spacecraft.
Reaction Engines Project Troy
The Reaction Engines Troy Mission is a concept of a future crewed mission to Mars. The concept arose to confirm the capability of the Skylon launch vehicle that it can and does enable large human exploration to the Solar System's planets.
The Troy spacecraft concept consists of an robotic precursor mission, including an Earth Departure Stage, and a Mars Transfer Stage. There is a habitation module, a storage module, and a propulsion module to be deployed from the spacecraft to land together at a selected site on the Martian surface to form a base. There are also ferry vehicles that would transfer crew members to and from the base to an orbiting crewed spacecraft. There would be three precursor spacecraft to Mars to set up three bases on the planet to enable maximum exploration of the planet's surface.
50 days after launch, the Earth Departure Stage is brought back to low Earth orbit by the Earth's gravity, and the Fluyt space tug would bring the stage back to the Orbital Base Station for construction of the later crewed mission.
The crewed spacecraft would consist of 3 habitation modules, 3 docking ports, and two ferry vehicles. The spacecraft would rotate along the centerline to provide artificial gravity. It would leave Earth with the Earth Departure Stage and transfer to Mars with the Mars Transfer Stage, and rendezvous with the precursor spacecraft in Martian orbit. The craft would dock together to enable the crew to transfer to the ferry vehicles for descent to the surface at a selected site. The crew, along with the equipped rovers, would spend 14 months to explore the Martian surface. The crew would return to Martian orbit with the ferry vehicle and rendezvous and dock with the orbiting crewed spacecraft. After a detailed inspection of the vehicle, the spacecraft would leave Mars for Earth on the Earth Return Stage. When the craft is captured in a Molniya orbit around Earth, the crew would board a ferry vehicle for transfer to low Earth orbit and rendezvous and dock with the waiting Skylon spacecraft for return to Earth.
Construction of the spacecraft would take place at the Orbital Base Station inside the cylindrical structure. Because the spacecraft is of highly modular design, the components would be brought up by the Skylon spacecraft. The rocket engines, fuel and oxidizer tanks, and habitation modules are sized to fit inside the Skylon payload bay, and that the fully assembled craft would also fit inside the cylindrical structure of the OBS.
The Fluyt Orbital Transfer Vehicle is a concept of a future space tug. It would have the ability to dock with orbiting spacecraft and move payload in orbit. It is conceived to be assembled from two parts, each sized to fit inside the Skylon payload bay, it would be launched from the Skylon and would also be an integral part for the construction of the Orbital Base Station as well as the Reaction Engines Troy and the retrieval of the Earth Departure Stage from the Precursor mission of the Troy mission.
|Wikinews has related news: UK firm designs hypersonic passenger jet|
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- "Hypersonic passenger jet designed". BBC News. 5 February 2008. Retrieved 2009-04-15.
- Jason Ford. "ARFL confirms feasibility of Reaction Engines' SABRE engine concept". The Engineer. Archived from the original on 11 August 2016. Retrieved 29 September 2017.
- "Reaction Engines Awarded DARPA Contract to Perform High-Temperature Testing of the SABRE Precooler" (Press release). 25 September 2017. Archived from the original on 28 September 2017. Retrieved 27 September 2017.
- "Passenger module study for Reaction Engines Skylon". Reactionengines.co.uk. Archived from the original on 15 June 2012. Retrieved 1 July 2016.
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- "Video on TROY Mission to Mars". Reactionengines.co.uk. Archived from the original on 26 June 2016. Retrieved 1 July 2016.
- "The Fluyt OTV". Reactionengines.co.uk. Archived from the original on 5 July 2012. Retrieved 1 July 2016.
- IAC-10.D2.3.7 - The Fluyt Stage: A Design for a Space-Based Orbit Transfer Vehicle
- Varvill, Richard; Bond, Alan (May 1993). "Skylon: A Key Element of a Future Space Transportation System". Spaceflight. Vol. 35 no. 5. London: British Interplanetary Society. pp. 162–166. ISSN 0038-6340.
- Bond, Alan; Varvill, Richard (April 2003). "SKYLON- a realistic single stage spaceplane". Spaceflight. Vol. 45 no. 4. London: British Interplanetary Society. pp. 158–161. ISSN 0038-6340.
- Varvill, Richard; Bond, Alan (2003). "A Comparison of Propulsions Concepts for SSTO Reusable launchers" (PDF). Journal of the British Interplanetary Society. 56: 108–17. Bibcode:2003JBIS...56..108V. Archived from the original (PDF) on 28 June 2012.
- Varvill, Richard; Bond, Alan (2004). "The SKYLON Spaceplane" (PDF). Journal of the British Interplanetary Society. 57: 22–32. Bibcode:2004JBIS...57...22V. Archived from the original (PDF) on 16 May 2011.
- House of Commons Science and Technology Committee (2007). "2007: A Space Policy - Seventh Report of Session 2006-08". II. Her Majesty's Stationery Office. ISBN 978-0-215-03509-7.
- Tony Martin, ed. (11 September 2008). Solar Power Satellites and Spaceplanes — The Skylon Initiative (Technical report). Reaction Engines Ltd.
- Varvill, Richard (2008). Heat Exchanger Development at Reaction Engines Ltd (IAC-08-C4.5.2) (PDF). 57th International Astronautical Congress. Archived from the original (PDF) on 25 July 2011.
- Varvill, Richard; Paniagua, Guillermo; Kato, Hiromasa; Thatcher, Mark (2008). Design and Testing of the Contra-rotating Turbine for the Scimitar Pre-cooled Mach 5 Cruise Engine (IAC-08-C4.5.3) (PDF). 57th International Astronautical Congress. Archived from the original (PDF) on 20 October 2011.
- Varvill, Richard; Bond, Alan (2008). "The SKYLON Spaceplane - Progress to Realisation" (PDF). Journal of the British Interplanetary Society. 61: 412–418. Bibcode:2008JBIS...61..412V. Archived from the original (PDF) on 12 February 2012.
- Hempsell, Mark; Longstaff, Roger (2009). "Skylon User Manual v1.1" (PDF). Reaction Engines Ltd. Archived from the original (PDF) on 18 April 2016.
- Hempsell, Mark; Longstaff, Roger (October 2011). The Requirement Generation Process for the SKYLON Launch System (IAC-09.D2.5.7). 60th International Astronautical Congress. Daejeon.
- Hempsell, Mark; Bond, Alan; Bond, R; Varvill, Richard (October 2011). Progress on the SKYLON and SABRE Development Programme (IAC-11.D 2.4.2, IAC-11.B3.2.6). 62nd International Astronautical Congress. Cape Town.
- Bond, Alan (8 December 2011). Progress on the SKYLON Reusable Spaceplane (PDF). 7th Appleton Space Conference (RALSpace).
- Hempsell, Mark (September 2013). Progress on SKYLON and SABRE (IAC-13.D2.4.6). 64th International Astronautical Congress. Beijing, China.
- Hempsell, Mark; Longstaff, Roger (2014). "Skylon User Manual v2.1" (PDF). Reaction Engines. pp. 1–52. Archived from the original (PDF) on 29 November 2015.
- Davis, Philippa; Hempsell, Mark; Varvill, Richard (2015). Progress On Skylon and SABRE (IAC-15-D2.1.8). 66th International Astronautical Congress.
- Reaction Engines Limited homepage
- Reaction Engines Talk to the Space Fellowship
- Mark Hempsell from REL appeared on The Space Show
- Guy Norris (Dec 18, 2017). "Reaction Begins Building U.S. Hypersonic Engine Test Site". Aviation Week Network.
- Guy Norris (Apr 11, 2018). "Boeing, Rolls-Royce Back Reaction Hypersonic Engine Developer". Aviation Week Network.