• BA-2100: A Bigelow module. Volume: 2,100 m3. Weight: 100 mT. Crew: 16, Cost: $500M.
• BA-330: A Bigelow module. Volume: 330 m3. Weight: 25 mT. Crew: 6. Cost: $125M.
• Falcon Heavy: An expendable launch vehicle from SpaceX. Payload: 53 mT. Cost: $150M.
• Propulsion Bus/Docking Node (PB/DN): A unit used to reboost the space station due to orbital decay coupled with a module that allows Bigelow modules to be attached together. Weight: 17 mT. Cost: $75M.
• Space Launch System Block I-A (SLS I-A): An expendable launch vehicle from NASA. Payload: 105 mT. Cost: $750M.
To live and work and be productive in space, you have to have a place to call home. While the Earth is certainly a great place to go home to (free air! free water! free – well, you get the point), it would become very expensive indeed if every time you knocked off your shift in space you took a ride back to Earth, and then got up the next day to fly back into space again! The obvious answer is to place your home, your city if you will, in space.
Shopping around for what’s available to use to build our city, we happily find Bigelow Aerospace, makers of the famous BA-330 and BA-2100 space station habitat modules (the names of the modules denote the pressurized volume of each unit). These inflatable modules go into space, where they, well, you know, inflate. Astronauts then move into what is essentially a balloon in space (aren’t all space modules really just that?). Ah, but what a balloon!
Crew capsules can dock at either end, and power is derived from solar panels, while excess heat is dumped into the biting cold of space using radiators. It even has windows! Home sweet home, indeed.
To launch these excellent habitat modules into space, we obviously need a launch vehicle. Once again, shopping around for what’s available to use to launch our city we find two Expendable Launch Vehicles (ELV). These rockets haven’t been built yet, but so long as funding continues they will be one day. The two ELVs are the SLS I-A and the Falcon Heavy.
Since the SLS I-A ELV can carry 105 mT into Low Earth Orbit (LEO), and one BA-2100 weighs 100 mT, it can carry only one unit at a time. We will call this the “BA-2100 Stack.”
The Falcon Heavy ELV can lift 53 mT to LEO, and each BA-330 weighs 25 mT, so it can carry 2 units at a time (assuming, of course, that it could fit in a payload shroud). We will call this the “BA-330 Stack.” The PB/DNs each weigh 17 mT, so 3 units will fly on the Falcon Heavy ELV to LEO. This will be called the “PB/DN Stack.”
Cost: (1) SLS IA + (1) BA-2100 = $750M + $500M = $1,250M
Weight: (1) BA-2100 = (1) 100 mT = 100 mT
Volume: (1) 2,100 m3 = 2,100 m3
Crew: (1) 16 = 16 Astronauts
(1) Falcon Heavy + (2) BA-2100 = $150M + (2) $125M = $400M
Weight: (2) BA-330 = (2) 25 mT = 50 mT
Volume: (2) 330 m3 = 660 m3
Crew: (2) 6 = 12 Astronauts
(1) Falcon Heavy + (3) PB/DN = $150M + (3) $75M = $375M
Weight: (3) 17 mT = 51 mT
So let’s build us a city in space, shall we? Hey, if the high school students at The Learning Community Charter School (www.tlcnm.net) in Albuquerque, New Mexico can have fun with this, then so can we.
The folks at Bigelow Aerospace have made it easy for us: they’ve already designed a very nice space station! It’s called the “Hercules Resupply Depot,” but we’ll just call it “Home.” Thanks, Bigelow!
As you can see from the poster, we’ll need three BA-2100s, six BA-330s, and three PB/DNs to complete the design. We can therefore calculate how many “stacks” we’ll need:
(3) BA-2100 = (3) BA-2100 Stacks
(3) $1,250M = $3,750M
(3) 100 mT = 300 mT
(3) 2,100 m3 = 6,300 m3
(3) 16 Crew = 48 Crew
(6) BA-330 = (3) BA-330 Stacks
(3) $400M = $1,200M
(6) 25 mT = 150 mT
(6) 330 m3 = 1,980 m3
(6) 6 Crew = 36 Crew
(3) PB/DN = (1) PB/DN Stack
(3) 17 mT = 51 mT
Adding everything up we get:
Total Cost: $5,325M
Total Weight: 501 mT
Total Volume: 8,280 m3
Total Crew: 84 Astronauts
Notice that our volume is close to the 8,300 cubic meters advertised in the Hercules image.
Currently, the International Space Station (I.S.S.) is orbiting the Earth, but will eventually be retired. There really is no comparison, however, in their home and ours:
Weight: 501 mT
Volume: 8,280 m3
Weight: 450 mT
Volume: 837 m3
While the two space station weights are nearly equal, the total volume is nearly ten (10) times the International Space Station with 14 times as many crew, all for 1/30th the cost. It’s keeping up with the Jones in reverse!
Maybe when the I.S.S. retires in the near future the international community can move on up to a bigger and better place that’s a wee bit more affordable, si?
For a more in-depth treatment of this high school project by Joe Maness & Rich Holtzin, visit www.stemfortheclassroom.com.