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I've been playing with Len Cormier's Bear Cub. As a tether
enthusiast, I'm interested in the impact of using a tether with the Bear Cub. A hanging tether can give as much as 800 m/s sub orbital grapple or trapeze target. The payload of the Bear Cub grows from 455 kg to about 1200 kg for such a tether. I use the rocket equation to get a table of the net velocity available to this configuration with increased payloads. This gave me the following table. Payload Ideal DV $/kg 455 9.472 549 620 9.233 403 900 8.865 278 1000 8.744 250 1200 8.516 208 Len estimated a per flight cost of about $250,000. I couldn't resist adding the cost per kilogram to this table. I'm a bit tentative about the conversion from "Ideal DV" to orbital altitude. If I use the Buzz Aldrin 15% loss to gravity, air resistance, etc. Then 9.474 km/s should produce an effective 8.23 km/s. If I spend 8.07 to get into a transfer orbit, and 0.16 to circularize the orbit, that looks like 550 km altitude. Does that work? Henry For sanity; these are the figures I used in my spreadsheet. Len gave an expected ideal DV for each of the pieces; the Tupelov carrier, the booster stage, and the orbiter. He quoted the ISP for the RL-10. The booster stage uses Kerosene, Len does not provide an ISP for the booster stage. I infer an exhaust of about 3200 m/s from the mass and DV. Payload Ideal DV ISP m/s Empty Fuel GLOW 455 5.553 4422 Orbiter 1945 6025 8425 3.249 3200 Booster 2340 19000 29765 0.670 Tupelov95 94400 Total 9.472 |
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