yhelothar
Lifer
- Dec 11, 2002
- 18,409
- 39
- 91
Holy moly
"its giant camera, which boasted a focal length of 77 inches, a 20-inch aperture"
aka... 2000mm F/4 lens
Oh oh oh! Pick me! I have a better idea! Let's stay here. Let's send robots out to explore space. Sending humans at this point is pointless. Robots can do it cheaper, and we don't have to worry about them getting back home.
Double NASA's budget and have them start doing things that give us a little more bang for the buck. Where's the James Webb Space Telescope? How about the DSCVR satellite? How about we send probes to a few of the water logged moons of the solar system and see if there's life there (before we contaminate all those places with life from Earth.) Answering that question - is there life elsewhere - is one of the most profound questions of mankind. Doing thousands of laps in a low earth orbiting space station is little more than theatrics.
Most rockets aren't able to throttle their engine. As far as I know the shuttle is the only launch systems that reduces power going through Max Q.
Also, are you sure about the SRBs? I have never heard of a throttleable solid rocket booster.
The following explanation is from T.R. Heppenheimer's "Development of the Space Shuttle 1972-1981," p. 176:
"The forward portion of each propellant charge was cast with a central perforation in the form of an eleven-point star, with the star's points being long and narrow. This allowed the thrust to vary as planned. The star initially exposed a large burning surface area, for peak thrust after liftoff. The burn spread from the points, widening them and reducing this burning surface. This lessened the thrust and hence the buildup in flight velocity, to prevent overstressing the vehicle through excessive aerodynamic pressure. the SSME's also helped by throttling back to 65 percent of rated power, to further diminish this pressure. Then, ascending amid thinner atmoshpere, the shuttle was free to accelerate anew. The star was completely consumed at fifty-two seconds, leaving a cylindrical perforation that would widen, for a useful increase in thrust."
