AEROSPACE VEHICLES

Brand	Owner (click to sort)	Address	Description
APOGEE	GATEWAY SPACE TRANSPORT, INC.	139 Brightfield Drive Ballwin MO 63021	Aerospace vehicles;
BLUE ORIGIN	Blue, Inc.	21218- 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft;
ELECTRON	Rocket Lab USA, Inc.	3881 McGowen Street Long Beach CA 90808	Aerospace vehicles, namely, rockets; Launch vehicles used to launch space vehicles; Space vehicles, namely, rockets; moveable rocket launching platform in the nature of a trailer; Rocket motor driven space vehicles, namely, rockets; Rocket propelled space vehicles, namely, rockets;
GRADATIM FEROCITER	Blue, Inc.	21218- 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft;
GRADATIM FEROCITER	Blue, Inc.	21218- 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft;
GRADATIM FEROCITER	Blue, Inc.	21218- 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft;
GRADATIM FEROCITER	Blue Origin	21218 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft;
LAUNCH. LAND. REPEAT.	Blue Origin	21218 76th Ave South Kent WA 98032	Aerospace vehicles, namely, launch vehicles and spacecraft; Aerospace vehicle parts, namely, rockets for use with aerospace vehicles;
ORION AEROSPACE	Bellanca, Derek	501 Fireberry Drive Fate TX 75087	Aerospace vehicles, namely, space launch vehicles; space launch vehicles, namely, self-propelled rockets; and spaceplanes;AEROSPACE;
	Where the owner name is not linked, that owner no longer owns the brand

Technical Examples

Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system can further include a movable control surface coupled to the fuselage and extending generally in a horizontal plane. The control surface can be movable to a deflected position in which the control surface can be positioned to create a flow pattern proximate to the fuselage when the aerospace vehicle is located in a flow field. The flow pattern can be positioned to create a pressure differential between the first portion of the fuselage and the second portion of the fuselage. The first and second portions can be located so that the pressure differential produces a yawing moment on the aerospace vehicle.