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Company News
The D1 redesign of SKYLON is progressing well. The preliminary trajectory analysis has been fed into a preliminary configuration analysis to establish how the vehicle will be trimmed in aerodynamic flight. This is the start of an iterative cycle of performance analysis and configuration definition with increasing refinement and detail which will lead to the final D1 definition.
Work has started on the payload provision based on the interfaces proposed in Revision 1 of the SKYLON Users’ Manual. The public consultation produced no suggestions for any changes whatsoever (which was a bit of a surprise) so as a consequence those interfaces are now being worked into the D1 vehicle design.
Work also started on defining D1’s Auxiliary Propulsion System. This system performs many functions on SKYLON; orbit manoeuvring, reaction control, the supply reactants to both the fuel cells and hydraulic power unit, and heat absorption during re-entry. As part of this work, Lolan Naicker of Cranfield University will conduct a postgraduate research project as part of his MSc Astronautics and Space Engineering looking at the SOMA engine which provides SKYLON’s orbit manoeuvring propulsion.
The first firm results from the Reaction Engines trade mission to the USA (as reported last month) came in February with the placing of a small study contract with the Physical Science Laboratory at the New Mexico State University. NMSU will be undertaking a preliminary evaluation of the requirements that SKYLON D1 will need to meet for safe autonomous flight based on their extensive heritage with unmanned flight vehicles, their expert knowledge of the US National Airspace System, and their expertise and experience in the Global Airspace System.
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