originally posted by: Zaphod58
a reply to: grey580
Dale Brown, years ago, started using what he called NiRTSATs, or Need it Right This Second Satellites. Same idea. They were small groups of cubesats
launched from a carrier aircraft, in the books it was a DC-10.
It was a good idea on paper, and a better idea in reality.
...
As an idea I have been exploring during my work breaks, and using a 3D model (i.e. on Maya
Xsi, Corel Draw and other CAD/CAM/FAE software), I think it is NOW possible for a
Non-NASA Commercial Operator to use
The CURRENT and very publicly available
Plans for the SPACE SHUTTLE and import
Them directly into a CAD/CAM program.
Then apply Aerodynamic, Thermodynamic,
Hull Torsion, Shear, Tensile and Compressive
Load testing on all that 1970's era space shuttle
hull and interior components using that fancy
Software so that an ALGORITHMICALLY optimized
hull and interior structure is created that can be
then 3D machined and robotically welded
using high-strength but relatively inexpensive
8000 series aluminum.
With 3D printed aluminum oxide ceramic composite heat shield plates created using
A two-layer symmetric hexagonal plating system,
I think the cost of building the shuttle itself
Can be easily reduced to less than
Ten Million dollars IF as much 3D printing
And CNC machining and robotic welding
As possible is used.
The technical term is:
"Design For Easy and Fast Manufacturability"
This REALLY reduces costs significantly if your
CAD/CAM/FEA software can do the optimization
Necessary. I suggest using CATIA for the design
Portion and Midas NFX for the Structures Stress
analysis and parts engineering/manufacturabilty
analysis. Using these software systems will save
HUGE MONEY down the line during 3D printing
and final shuttle/booster assembly.
To further reduce costs use a mobile sea launch
Platform such as a used but modified semi-sub
floating oil rig platform and launch in international waters on an equatorial plane.
Flight control could use true real-time Linux OS
that's certified for critical systems and a full autopilot using a combined GPS and inertial
guidance system for launch and orbit, a fully
Automated robotic payload delivery system
and then possibly a Pure vision recognition
for final landing at an airstrip. No Astronauts
At all...it's basically a spaceplane drone to
Save as much launch cost as possible!
The Launch rocket itself SHOULD use the
same design as the 1960's era Saturn V F1-series
Motors but do a Finite Element Analysis to simplify
and stress analyze all the parts ...then machine
them out of high temp ceramic composite for use
with relatively simple, cheap but effective
Hydrogen/LOX fuel and oxidizer combo! That would cost another ten million to build but the
total cost of launch shouldn't be more than
5-to-7 million per launch which is MUCH CHEAPER than even a 50 million bucks a launch for today's
Cheapest system of say Boeing Sea Launch.
Even the launch rocket itself could be made re-usable IF all its major components use
8000 series Aluminum and High temp
Alumina-ceramic composite.
Those F1 motors could do over a million pounds of thrust. Using a cluster of them under a single large
Reusable and Combined Hydrogen/LOX tank and
Combo booster would save a lot of money!
Nowadays a commercial operator could do this
For a less than 30 million dollar initial investment!
edit on 2015/8/10 by StargateSG7 because: sp
edit on 2015/8/10 by
StargateSG7 because: sp
edit on 2015/8/10 by StargateSG7 because: sp
edit on 2015/8/10 by StargateSG7 because:
sp