Structure and method for controlling inlet shock position of...

Details Structure and method for controlling inlet shock position of... Structure and method for controlling inlet shock position of...

2005-04-19

2005-04-19

Gartenberg, Ehud (Department: 3746)

Power plants

Reaction motor

Air supplied by ram effect

C137S015200

Reexamination Certificate

active

06880342

ABSTRACT:
System and method for controlling inlet shock position and airflow Mach number of a hypersonic vehicle is described wherein thermally controlled fuel is controllably injected into the airflow at the inlet of the propulsion system of the vehicle.

REFERENCES:
patent: 3086357 (1963-04-01), Rubin
patent: 4749151 (1988-06-01), Ball et al.
patent: 5085048 (1992-02-01), Kutschenreuter et al.
patent: 6715293 (2004-04-01), Sillence et al.

Affiliated with

Also associated with

Rating

Structure and method for controlling inlet shock position of... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Structure and method for controlling inlet shock position of..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Structure and method for controlling inlet shock position of... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3368437