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Aerospike engine to be tested at high altitude (Finally!)
The new start-up Arca Space Corporation will test this year for the very
first time, more than 50 years after the aerospike was developed, the high altitude performance of an aerospike on their liquid-fueled demonstrator for their planned SSTO: Flight of the Aerospike: Episode 1. https://www.youtube.com/watch?v=L1hnImvI2gw ARCA to perform historic space flight of aerospike engine. Published by Klaus Schmidt on Sat Jun 17, 2017 9:30 am Quote:
Rocket engine nozzles now are of a fixed bell shape. However, it is known a bell nozzle is most efficient at a certain altitude and less efficient at other altitudes. As an example, the SpaceX Merin engines for sea level use have an Isp of 312 s. But the Merlin Vacuum optimized for vacuum use given a much longer nozzle has a vacuum Isp of 348 s. Since all orbital rockets operate in stages, this lack of efficiency at varying altitudes was considered acceptable. But the SSTO concept (single-stage-to-orbit) would use a single engine all the way to orbit. So there were investigated methods such as the aerospike that could maintain high efficiency at all altitudes. However, it came to be believed that SSTO's were not feasible, either technically or economically. So little research went into the aerospike. This is extremely unfortunate. In fact, the aerospike can increase payload for all rockets including staged ones. If the aerospike or other altitude compensation had been used for existing rockets, it would have been observed that at the increased Isp, several *existing* first stages could be SSTO's. For instance, the famous Saturn 1C first stage of the of the Saturn V could be SSTO with altitude compensation to give it a max vacuum Isp of 360 s instead of its 304 s. As I said this increase in payload using the aerospike can be significant. I estimated it could be 25% for the Falcon 9. How much is the increase is dependent on the individual rocket. But for a solid rocket launch system I was investigating I found the aerospike doubled the payload to orbit! This is because solid rocket motors typically get about 285 s vacuum ISP. But using a rocket simulation program, I found the vacuum Isp could get as as high as 325 s and above. The required bell size though would be quite large, and would extend far outside the width of the rocket body, making it impractical. But the aerospike could do this without extending outside the rocket body's width. In short the reason why the aerospike hasn't been used for any rocket liquid or solid is because of the idea it is only useful for SSTO's and because of the idea that SSTO's aren't useful. Both of these ideas are incorrect. Bob Clark ---------------------------------------------------------------------------------------------------------------------------------- Finally, nanotechnology can now fulfill its potential to revolutionize 21st-century technology, from the space elevator, to private, orbital launchers, to 'flying cars'. This crowdfunding campaign is to prove it: Nanotech: from air to space. https://www.indiegogo.com/projects/n...ce/x/13319568/ ---------------------------------------------------------------------------------------------------------------------------------- |
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