Super High Altitude Research Project

The Super High Altitude Research Project (Super HARP, SHARP) was a U.S. government project conducting research into the firing of high-velocity projectiles high into the atmosphere using a two stage light gas gun, with the ultimate goal of propelling satellites into Earth orbit. Design work on the prototype space gun began as early as 1985 at the Lawrence Livermore National Laboratory in California and became operational in December 1992.[1] It is the largest gas gun in the world.[2]

Contents

Design and operation

Rather than a single straight barrel, the SHARP gun is actually of an L-shape design comprising 2 separate sections—a 270 ft (82 m) long steel combustion section & pump tube, and a 155 ft (47 m) long launch tube (or barrel)—joined together at a right angle. At each end of the pump tube, there sits a 100-ton rail-mounted sled to absorb recoil energy from firing. A smaller 10-ton sled is also mounted on a set of tracks at the aft-end of the launch-tube near the junction point.[2]

The firing sequence begins with the ignition of a methane gas mixture in the combustion section at the far end of the pump tube, which has been filled with pressurized hydrogen gas. The resultant explosion drives a 1-ton steel piston down the pump tube towards the junction point, rapidly compressing the hydrogen gas in the pump tube to a pressure of 60,000 psi (4,100 atm). Meanwhile, a small projectile rests in the adjacent depressurized launch tube. As the hydrogen gas reaches maximum pressure, a coupling holding the projectile in place is destroyed, driving the projectile down a 4-in diameter barrel at extremely high velocities until it bursts through a thin plastic sheet covering the end of the gun. All recoil forces are absorbed by the rail-mounted sleds as they are propelled outwards along their tracks.[2]

Tests and cancellation

Headed by John Hunter, the SHARP gun fired projectiles using expanding hydrogen and achieved velocities of 3 km/s (6,700 mph) or Mach 8.8 for 5 kg (11 lb) projectiles. Had the project continued, there were plans to elevate the tube and begin space launch trials potentially reaching speeds of up to 7 km/s (16,000 mph), or about Mach 21.[1]

The tests were designed as a precursor to the "Jules Verne Launcher," an even larger light gas gun with a 3,500 m (11,500 ft) barrel length designed in the early 1990s[1] for first-stage satellite launch. This was to cost $1 billion, but funding was not forthcoming and the project was eventually canceled in 1995. However, the SHARP gun continued to be used for high-speed tests in other areas of research, such as scramjet development.[1]

The concept of ballistic escape velocity is well proven. The largest challenge is maintaining such high velocities, because air resistance and aerothermal heating will significantly slow down any such object.

See also

References

  1. ^ a b c Wade, Mark. "SHARP at Encyclopedia Astronautica". http://www.astronautix.com/lvs/sharp.htm. Retrieved 2009-09-03. 
  2. ^ a b c "The Jules Verne Gun". Popular Science (Hearst Communications, Inc.). April 1998. http://www.popularmechanics.com/science/air_space/1277296.html?page=1. Retrieved 2009-09-03. 

External links