Skylon (spacecraft)

Skylon
Artist's concept of a Skylon reaching orbit.
General information
Type	Reusable spaceplane
National origin	United Kingdom
Designer	Reaction Engines Limited
Status	Under development
History
Developed from	HOTOL (Horizontal Take-Off and Landing) project

Skylon is a series of concept designs for a reusable single-stage-to-orbit spaceplane by the British company Reaction Engines Limited (Reaction), using SABRE, a combined-cycle, air-breathing rocket propulsion system.

The vehicle design is for a hydrogen-fuelled aircraft that would take off from a specially built reinforced runway, and accelerate to Mach 5.4 at 26 kilometres (85,000 ft) altitude (compared to typical airliner's 9–13 kilometres or 30,000–40,000 feet) using the atmosphere's oxygen before switching the engines to use the internal liquid oxygen (LOX) supply to accelerate to the Mach 25 necessary to reach a 400 km orbit.^[1]

It would carry 17 tonnes (37,000 lb) of cargo to an equatorial low Earth orbit (LEO); up to 11 tonnes (24,000 lb) to the International Space Station, almost 45% more than the capacity of the European Space Agency's Automated Transfer Vehicle;^[2] or 7.3 tonnes (16,000 lb) to Geosynchronous Transfer Orbit (GTO),^{[citation needed]} over 24% more than SpaceX Falcon 9 launch vehicle in reusable mode (as of 2018^{[update][3][4]}).

The relatively light vehicle would re-enter the atmosphere and land on a runway, being protected from the conditions of re-entry by a ceramic matrix composite skin. When on the ground, it would undergo inspection and necessary maintenance, with a turnaround time of approximately two days, and be able to complete at least 200 orbital flights per vehicle.

As work on the project has progressed, information has been published on a number of design versions, including A4,^[5] C1,^[6] C2,^[7] and D1.^[8] Testing of the key technologies was successfully completed in November 2012, allowing Skylon's design to advance from its research phase to a development phase.^[9][10] As of 2021^[update], the groundworks for an engine test facility have been completed at Westcott. While plans to be performing uncrewed test flights in a "hypersonic testbed" (HTB) by 2025^[11] now look dubious, the Wescott test facility is complete, and they have completed an all-up engine test at mach 3.5; which meets or exceeds the SR-71's still standing airspeed record.[^[12]

In paper studies, the cost per kilogram (kg) of payload carried to LEO in this way is hoped to be reduced from the current £1,108/kg (as of December 2015^[update]),^[13] including research and development, to around £650/kg (718.16USD/Kg), with costs expected to fall much more over time after initial expenditures have amortised.^[14] In 2004, the developer estimated the total lifetime cost of the Skylon C1 programme to be about $12 billion.^[14] As of 2017^[update], only a small portion of the funding required to develop and build Skylon had been secured. For the first couple of decades the work was privately funded, with public funding beginning in 2009 through a European Space Agency (ESA) contract. The British government pledged £60 million to the project on 16 July 2013 to allow a prototype of the SABRE engine to be built;^[15] contracts for this funding were signed in 2015.