US 3,943,656 AGranted

Two stage rocket with pressure responsive means for frictionally engaging second stage

AssigneeDamon Corporation

InventorCharles J. Green

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Abstract

A toy rocket has a motor receptacle designed to receive a rocket motor of the type fueled by a self-pressurizing liquid propellant. The rocket motor during the fueling operation has its nozzle seated in a launcher through which liquid propellant flows into the propellant cavity of the rocket motor. When the propellant cavity of the rocket motor is pressurized, a member responsive to propellant pressure in the rocket motor engages a portion of the walls of the motor receptacle in the rocket body. When the pressure responsive member releases the receptacle walls, relative motion is provided between at least a portion of the rocket body and the rocket motor. For example, in one embodiment of the toy rocket, a second stage portion of the rocket is spring-biased away from a first stage portion of the rocket body. The major section of the rocket motor is fixed to the first stage portion. The pressure responsive member on the rocket motor engages the second stage portion while the rocket motor contains propellant to prevent separation of the first and second stages. When the propellant is expended, the pressure responsive member releases the second stage, allowing separation of the second stage from the first stage. A parachute is then deployed from the second stage to brake the descent of the rocket.

Claims6

Dependent claims

A toy rocket comprising:

a first stage having a body housing a rocket motor, said motor comprising:
a motor body having means defining a propellent cavity for receiving and holding a pressurized propellent fluid, and also defining a second cavity for receiving and holding a pressurizing gas, said motor body having means communicating between said second cavity and the exterior thereof including at least one aperture extending through a peripheral wall of said second cavity;
a nozzle connected to said motor body and communicating between said propellant cavity and the exterior of said motor;
pressure responsive means for sealing said communicating means and said second cavity when it is pressurized, said pressure responsive means comprising a member of flexible, resilient material disposed across said aperture on the inside of a peripheral wall of said second cavity and being capable of extending through said aperture in response to pressure increases within said second cavity;
the propellant cavity means including a flow channel in fluid communication between said propellent cavity and said second cavity;
and
means for restricting fluid passage through said flow channel, including a restriction member, said restriction member being pervious to gas and substantially impervious to liquid;
a second stage having a body portion adjacent said second cavity exterior, said pressure responsive means frictionally engaging said second stage body portion through said aperture when said second cavity is pressurized. pg,16

5 more elements

Dependencies are inferred from the claim text.