Hypersonic aircraft surface pressure measuring device and pressure guide pipeline connecting method thereof

The invention relates to the field of hypersonic aircraft flight measurement, and discloses a hypersonic aircraft surface pressure measuring device and a pressure guide pipeline connecting method thereof. The hypersonic aircraft surface pressure measuring device comprises a plurality of pressure measuring holes formed in the surface of a flight vehicle shell, wherein the shell is further providedwith mounting holes coaxially communicated with the pressure measuring holes; a pressure measuring nozzle is arranged in the pressure measuring hole; the front end of the pressure measuring nozzle iscommunicated with the pressure measuring hole, and a metal pressure guide pipe is arranged at the rear end of the pressure measuring nozzle; the outer wall of the metal pressure guide pipe is sleevedwith a PVC hose; and the PVC hose is communicated with the electronic pressure scanning valve through a Teflon hose. For the hypersonic aircraft surface pressure measuring device, the pressure guide pipeline is firm in connecti