CPSS StarBooster 200

hesham

ACCESS: USAP
Senior Member
Joined
26 May 2006
Messages
33,481
Reaction score
13,530
Hi,

http://www.calpoly.edu/~aero/news/9900.pdf
 

Attachments

  • StarBooster 200.JPG
    StarBooster 200.JPG
    65.2 KB · Views: 138
I like very much this project.

The whole website here
http://www.starbooster.com

It hadn't been upgraded since june 2004 until recently. Seems Buzz Aldrin added some stuff late may...
 
From NASA;
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19990113117_1999192503.pdf
 

Attachments

  • STARBOOSTER.JPG
    STARBOOSTER.JPG
    31.4 KB · Views: 65
  • EARLY CONCEPT.JPG
    EARLY CONCEPT.JPG
    21.3 KB · Views: 68
  • CURRENT DESIGN.JPG
    CURRENT DESIGN.JPG
    19.7 KB · Views: 54
  • STARBIRD.JPG
    STARBIRD.JPG
    12.8 KB · Views: 74
It's interesting to note some of the conclusions from the starbooster studies. If staging occurs at Mach 3, a heat-sink structure is sufficient, and the vehicle has sufficient energy and L/D to glide back to base without turbofans. Staging between Mach 3 and Mach 6 requires turbofans and additional TPS.

But the Starbooster studies weren't the end-all for theoretical work on reusable first stages. AFRL Air Vehicles Directorate is fleshing out its concept for a flyback booster (X-54?) that will stage at Mach 6.5 and return to base using a derivative of the shuttle "Return to Launch Site" maneuver. It will take a lot of funding to make it happen, but the concept seems sound to me.
 
Hi,

http://www.spaceandtech.com/spacedata/rlvs/starbooster_sum.shtml
 

Attachments

  • 1.JPG
    1.JPG
    38.5 KB · Views: 54
  • StarBoosterFamily.jpg
    StarBoosterFamily.jpg
    19.7 KB · Views: 68
Hi,

the StarBooster 200.
 

Attachments

  • sb200accel.jpg
    sb200accel.jpg
    40.8 KB · Views: 50

Please donate to support the forum.

Back
Top Bottom