Projectile accelerator with heatable barrel
View Patent ↗Systems, methods, and apparatuses are described for accelerating projectiles at high velocity. A barrel may include one or more heaters configured to heat a bore of the barrel prior to launch of a projectile. The barrel bore may be formed in a tungsten sleeve and may be heated to high temperatures. Heat from the barrel bore may be transferred to expanding propellant behind a projectile as it travels through the barrel bore.
1. An apparatus comprising:
a barrel comprising a bore extending from a barrel entrance to a barrel exit positioned forward of the barrel entrance, and further comprising a heater configured to heat at least a surface of the bore;
a shutter, positioned proximate to the barrel exit, having an open configuration exposing the bore and a closed configuration preventing passage of gas into or out of the bore;
a breach chamber positioned behind the barrel entrance;
a sealable compression chamber positioned behind the breach chamber; and
a gas supply coupled to the compression chamber via a valve openable to allow delivery of gas into the compression chamber and closeable to prevent release, via the valve, of gas in the compression chamber.
2. The apparatus of claim 1 , wherein the gas supply comprises a supply of a light gas comprising one or more of hydrogen and helium.
3. The apparatus of claim 1 , further comprising a recovery manifold coupled to the bore and to the gas supply.
4. The apparatus of claim 1 , further comprising a projectile positioned in the breach chamber, wherein the projectile is sized to pass through the bore.
5. The apparatus of claim 1 , wherein the heater comprises a plurality of individually-controllable heaters distributed along at least a portion of a length of the barrel.
6. The apparatus of claim 1 , further comprising a projectile, formed from compressed dust, in the breach chamber.
7. The apparatus of claim 1 , wherein the barrel comprises a tungsten sleeve.
8. The apparatus of claim 1 , further comprising:
a second shutter, positioned behind the barrel entrance, having an open configuration exposing the bore and a closed configuration preventing passage of gas into or out of the bore.
9. An apparatus comprising:
a barrel comprising a bore extending from a barrel entrance to a barrel exit positioned forward of the barrel entrance, and further comprising a plurality of individually-controllable heaters, distributed along at least a portion of a length of the barrel, configured to heat at least a surface of the bore;
a breach chamber positioned behind the barrel entrance;
a sealable compression chamber positioned behind the breach chamber; and
a gas supply coupled to the compression chamber via a valve openable to allow delivery of gas into the compression chamber and closeable to prevent release, via the valve, of gas in the compression chamber.
10. The apparatus of claim 9 , further comprising:
a first shutter, positioned forward of the barrel exit, having an open configuration exposing the bore and a closed configuration preventing passage of gas into or out of the bore; and
a second shutter, positioned behind the barrel entrance, having an open configuration exposing the bore and a closed configuration preventing passage of gas into or out of the bore.
11. The apparatus of claim 9 , wherein the gas supply comprises a supply of a light gas comprising one or more of hydrogen and helium.
12. The apparatus of claim 9 , further comprising a recovery manifold coupled to the bore and to the gas supply.
13. The apparatus of claim 9 , further comprising a projectile positioned in the breach chamber, wherein the projectile is sized to pass through the bore.
14. The apparatus of claim 9 , further comprising a projectile, formed from compressed dust, in the breach chamber.
15. The apparatus of claim 9 , wherein the barrel comprises a tungsten sleeve.
16. A method comprising:
heating, using one or more heaters positioned external to a bore of a barrel, a surface of the bore, wherein the barrel comprises a barrel entrance and a barrel exit positioned forward of the barrel entrance, and wherein the bore extends from the barrel entrance to the barrel exit;
placing a projectile in a breach chamber positioned behind the barrel entrance;
pressurizing, in a compression chamber, a propellant gas; and
accelerating, by release of the pressurized propellant gas from the compression chamber into the breach chamber, and while the surface of the bore is heated using the one or more heaters, the projectile from the breach chamber and through the bore.
17. The method of claim 16 , wherein the one or more heaters comprise a plurality of individually-controllable heaters distributed along at least a portion of a length of the barrel, and wherein the heating comprises heating a first portion of the bore surface to a first temperature and a second portion of the bore surface, positioned closer to the breach chamber, to a second temperature different than the first temperature.
18. The method of claim 16 , further comprising:
closing, after exit of the projectile from the bore, a shutter positioned proximate to the barrel exit, wherein the closed shutter prevents passage of gas into or out of the bore.
19. The method of claim 16 , further comprising:
recovering, after passage of the projectile through the bore, the propellant gas.
20. The method of claim 16 , wherein the pressurizing comprises one or more of:
mechanically reducing a volume of the compression chamber,
creating an electrical arc in the compression chamber, or
injecting plasma into the compression chamber.