Rocket Exhaust Probe.
Patent, Filed 10 Jan 86, patented 5 May 87,
DEPARTMENT OF THE AIR FORCE WASHINGTON DC
Pagination or Media Count:
A rocket exhaust probe 10 for collecting particulates from a rocket exhaust plume. The probe comprises a tungsten nose tip 18, a tip holder 20, a probe body 22 and a tail section 24. Rocket exhaust gas enters the probe at the nost tip inlet 32 and passes into a mixing chamber 36 where the exhaust gas mixes with an exhaust gas. The mixture of exhaust gas and inert gas then passes into a diffusion chamber 50 where if further cools and decelerates before passing throudh a submicron particle collection 52.
- Combustion and Ignition
- Test Facilities, Equipment and Methods
- Rocket Engines