RocketSTEM Issue #5 - January 2014 | Page 55

As an example of the applicability of REL’s SABRE engine and heat exchanger technology to Mach 5 cruise, REL and the European Union are exploring a new aircraft called LAPCAT. It would use the Scimitar pre-cooled engine - a derivative SABRE engine - which would allow I for commercial flights between Brussels and Sydney - a distance of 18,700 km (11,600 miles) in less than five hours. mage: Reaction Engines and material tolerances to extreme environmental variables are crucial factors and the lightweight heat exchangers appear to solve these critical problems. During 1989-2000 work focused on the development of the SABRE engine and the final Skylon launch vehicle. Innovations in aerothermodynamics, propulsion and control technology attracted a great amount of interest, private investment and finally government support. The innovative carbon fibre reinforced plastic fuselage for Skylon provides a strong yet lightweight airframe, surrounded by a single skin of material, a ceramic external aeroshell. This is corrugated for stiffness and thermal compliance on the substructure upon which it is mounted. A thorough research programme followed, demonstrating the techniques for full scale heat exchangers and the manufacturing techniques to build these components. ESA independently reviewed the work performed by Bond and REL for the UK government, removing any technical concerns and largely validating Bond’s approach. In 2011 ESA reported the following to the UK Space Agency: “ESA are confident that a ground test of a sub-scale [SABRE] engine can be successfully performed to demonstrate the flight regime and cycle and will be a critical milestone in the development of this program and a major breakthrough in propulsion worldwide.” Return to flight The UK government and the UK Space Agency had removed themselves from the launch technology game following the Thatcher government’s notional withdrawal from UK space efforts in the 1980s. However in early 2012, buoyed by ESA’s recommendations, Bond and REL began testing the first full scale SABRE pre cooler with a jet engine to test heat exchanger performance in a working environment. This demonstration pre-cooler included over 50 kilometres of heat exchanger tubing weighing less than 50 kilogrammes and dropped the air temperature to minus 150 degrees Celsius in 20 milliseconds. In November 2012 REL announced successful completion of the SABRE engine tests with its pre-cooler heat exchanger and ESA gave its official validation of the results which was backed up by the UK Minister for Universities and Science David Willetts. Willetts has earmarked SABRE and Skylon as a “high priority” technology project and is working with the UK’s Department of Transportation to allow Skylon flights within UK airspace. Bond himself has said; “These successful tests represent a fundamental breakthrough in propulsion technology. Reaction Engines’ lightweight heat exchangers are going to force a radical re-think of the design of the underlying thermodynamic cycles of aerospace engines. These new cycles will open up completely different operational characteristics such as high Mach cruise and low cost, re-usable space access, as the European Space Agency’s validation of Reaction Engines’ SABRE engine has confirmed. “The REL team has been trying to solve this problem for over 30 years and we’ve finally done it. Innovation doesn’t happen overnight. Independent experts 53 www.RocketSTEM.org 53