The Boom SST engine problem, Part 2

By Bjorn Fehrm

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Introduction

December 01, 2016, ©. Leeham Co: Boom Technology and Virgin Atlantic plan to offer supersonic business class passenger traffic over the Atlantic. We covered the number of challenges that this poses in recent articles. The most difficult challenge is finding a suitable engine.

We started the investigation into a suitable engine in the last article. A Supersonic Transport Aircraft (SST) needs an engine which is very different from the latest crop of high-performance airliner engines.

airplane-1

Figure 1. Boom Technologies Boom Mach 2.2 airliner with 45-seater. Source: Boom

The air entering the engine intake at Mach 2.2 is taken from standing still to a speed of 450m/s within a fraction of a meter. This raises the air pressure and temperature more than the combined intake/fan/low compressor does for a modern turbofan. The result is that the core’s high pressure compressor must adapt; it can’t have a high compression ratio (then things get too hot).

Add to that, that the engine must be slender. It can’t have a wide fan and therefore high by-pass ratio because the supersonic drag of such large engines would be too high.

Summary:

  • The SST engine must be based on a core with a low pressure ratio.
  • Such cores are no longer available in modern airliner engines.
  • One must use cores from the military field of supersonic engines.
  • We check what kind of engine can be constructed around such a core.
  • Is the Boom SST mission then possible with an engine done with an existing core?

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