Aerial vehicles

Claim 1

AN AERIAL RECONNAISSANCE VEHICLE COMPRISING A FIRST CYLINDRICAL ROCKET MISSILE HAVING A REAR PORTION INCLUDING A PROPULSION MEANS AT ITS REAR END, SAID PROPULSION MEANS LYING WITHIN THE CIRCULAR PERIPHERY OF THE MISSILE, AND A HOLLOW FRONT PORTION CONTAINING A SECOND ROCKET MISSILE WHICH IS DISPOSED WITH ITS NOSE POINTING TOWARDS THE REAR END OF THE FIRST MISSILE AND WHICH HAS A PROPULSION NOZZLE AT ITS REAR END; MEANS FOR SEPARATING THE REAR PART OF THE FIRST MISSILE FROM THE FRONT PART CONTAINING THE SECOND MISSILE; FIN MEANS ON THE REAR PORTION OF THE FIRST MISSILE FOR STRABLIZING THE FIRST MISSILE IN A SPINNING CONDITION; FURTHER FIN MEANS ON THE FRONT PORTION OF THE FIRST MISSILE FOR STABLIZING THE SAID FRONT PORTION IN A SPINNING CONDITION AFTER SEPARATION OF THE SAID REAR PORTION FROM THE SAID FRONT PORTION; A CAMERA MOUNTED IN THE FRONT OF THE SECOND MISSILE WITH ITS LENS POINTING LATERALLY AND SOMEWHAT TOWARDS THE FRONT END OF THE FIRST MISSILE; WINDOW MEANS IN FRONT OF THE CAMERA, AND GYRO-OPERATED MEANS FOR OPERATING THE CAMERA EACH TIME THE CAMERA LENS POINTS DOWNWARDS DURING THE DESCENT OF THE COMBINED FIRST AND SECOND MISSILES.