Patent ID: 11932424
Assignee: ROMAN NAWOJCZYK
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 1:
2. The system according to claim 1,
wherein each space rocket comprises: at least two spreadable arms located on the opposite sides of the fuselage;
wherein all spreadable arms are mounted on each fuselage top part;
wherein all spreadable-arms are suitably spaced out on each fuselage so that they could spread out on two sides;
wherein all spreadable arms are completely spread out and are transverse to the space rocket fuselage when are entirely lifted;
wherein all spreadable arms are alongside and adjacent the space rocket fuselage when are entirely lowered;
wherein all spreadable arms are configured to be lowered during an ascent phase of the space rocket;
wherein the at least two spreadable arms are configured to be at least partially lifted during a descent phase of the space rocket such that the spreadable arms provide aerodynamic braking to the space rocket;
wherein the at least two spreadable arms are configured to be fully lifted during a landing phase of the space rocket such that the at least two spreadable arms support said space rocket on two gantries, whereby said space rocket hangs on two gantries.