A commenter earlier brought up an interesting thought that’s been bugging me for a while. Bigelow is trying to build his 3-person Sundancer module to be light enough to launch on either a bare-bones Atlas V, or a single-stick Falcon IX (or a Soyuz for that matter). However, he’s not going to actually ramp up the available capacity to 9 people until 2012 when Nautilus is on-line. Now, this might actually make sense, if nobody is able to field a manned commercial vehicle with high enough flight rate to keep Sundancer busy until then. However, if someone is able to come up with a passenger transportation solution, it might be better for Bigelow to just crank out a few more Sundancer modules while he works on finishing up development on Nautilus. That way he can ramp up demand more smoothly, and benefit from higher flight rates (and hence lower ticket prices and more demand for his modules) sooner rather than later.
Sundancer is also conveniently small enough that it’d probably make sense to have more than one station in more than one orbit/inclination. A Sundancer module for instance might make a good core for a transportation node/fuel depot. By having the fuel depot man-tended, all of the Autonomous Rendezvous and Docking issues, as well as the automatic propellant feed coupling issues go away, as you can use man-in-the-loop controls to simplify the former, and could just manually connect couplings for the latter. Or you could see having one or two Sundancer modules used as free-flyers for microgravity research/production. Once every couple of weeks, a new supply ship would get there, tend the station, load and unload new experiments or raw materials/processed materials, perform any preventative maintenance needed, get the experiments started again (and do any debugging needed) and then close it back off and head home. Or if you had such a free-flyer in a close formation with a manned Sundancer station, you could ferry back and forth to the unmanned free-flyer if problems cropped up, without having to have people on-board continuously, which tends to greatly degrade the microgravity environment (us humans are clumsy louts).
Other uses could be like I mentioned previously, as “mission modules” for use with commercial capsules to allow for long-duration spaceflight. Combine this with a refueled upper stage of some sort (either a K-1 like I’ve discussed, or a Falcon IX upper stage like I talked about way back, or a refueled Centaur like LM has discussed), and you could very well have commercial translunar missions before the Block I CEV is even in service.
One other point I ought to discuss. As I mentioned in the other post (and previously in my writeup of my Bigelow visit):
While in there, I was able to pick the brain a bit of the engineer who was giving us the tour. I had been curious to find out if Bigelow was interested in doing subscale versions of the module for potential use in lunar transfer vehicles or other applications. The answer I was given was that Bigelow would probably be willing to work out some sort of a deal if there was sufficient interest. I also asked him what the current plans were for launching the station, since the reported weight of 50,000lbs puts it at the upper end of what current ELVs can deliver to orbit. He mentioned that they were looking at several options, including launching all at once on a Delta IV Heavy, or maybe a Proton, or even The Stick if it gets developed. He also mentioned that if those didn’t pan out, or if a lighter lift but more affordable booster was on the market, that they might launch it in several pieces and fit it out on orbit. As it is, there’s a decent amount of on-orbit fitting out anyhow for an inflatable module, so this isn’t as big of a hassle. A lot of the quoted weight is probably in the water bags used for radiation control, and in other internal pieces, so maybe flying it on three or four Falcon Vs might be possible. He didn’t state what the minimum mass they could break it down into was though.
One thing that means is that if Nautlius could be launched partially loaded, and then the rest of the gear brought up and installed on a second flight (possibly halving the required minimum launch weight), the same may hold true of Sundancer as well. Which means that it could possibly be launched mostly empty on a K-1 (if they become available), and then fitted out on a subsequent flight. Sundancer is also small enough that if you really can launch the thing empty, and then fit it out with subsequent flights, that makes using it as a lunar surface module a lot easier. Having a commercial lunar lander that can place 10klb on the surface or even 20klb is going to be far easier than a 45klb cargo lander.
As an old Role-Playing Game manual once said “the potential uses are limited only by the heights of your creativity, or the depths of your neurological disorders.”
Anyway, I think that although Sundancer is seen by Bigelow as a short of near-term solution to get some sort of destination up there, to start the ball rolling, I think that this design may very well have far more potential than that.
Latest posts by Jonathan Goff (see all)
- FISO Telecon Lecture on LEO Propellant Depots for Interplanetary Smallsat Launch - November 28, 2018
- AAS Paper Review: RAAN Agnostic 3-Burn Departure Methodology for Deep Space Missions from LEO Depots (Part 2 of 2) - September 17, 2018
- AAS Paper Review: RAAN Agnostic 3-Burn Departure Methodology for Deep Space Missions from LEO Depots (Part 1 of 2) - September 15, 2018