US 12,234,038 B2
Recoverable rocket and an associated recovery method
Jiantang Jiang, Zhongshan (CN)
Filed by Jiantang Jiang, Zhongshan (CN)
Filed on Jul. 21, 2023, as Appl. No. 18/356,394.
Claims priority of application No. 202310623827.7 (CN), filed on May 30, 2023.
Prior Publication US 2024/0208674 A1, Jun. 27, 2024
Int. Cl. B64G 1/62 (2006.01); B64G 1/00 (2006.01); B64G 1/40 (2006.01); F02K 9/62 (2006.01); F02K 9/74 (2006.01); F02K 9/78 (2006.01)
CPC B64G 1/006 (2023.08) [B64G 1/401 (2013.01); B64G 1/62 (2013.01); B64G 1/623 (2023.08); F02K 9/62 (2013.01); F02K 9/74 (2013.01); F02K 9/78 (2013.01)] 13 Claims
OG exemplary drawing
 
1. A recoverable rocket comprising:
a recoverable rocket comprising a rocket body and at least two side wings, wherein:
one end of each side wing is connected to a casing of the rocket body, and the other end is connected to a deceleration mechanism; the deceleration mechanism comprises a turbine engine and a propeller; the turbine engine is connected to the rocket body through ducts arranged in the side wing, and the rocket body supplies the energy required for the turbine engine to work; the propeller is arranged below the turbine engine, the propeller is connected to a drive shaft of the turbine engine, and the turbine engine drives the propeller to rotate in the air to generate a thrust which decelerates the rocket during recovery; the rocket body comprises a structural system, a propulsion system, a control system and a set of landing legs.