The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 19, 2024

Filed:

Aug. 14, 2019
Applicant:

Israel Aerospace Industries Ltd., Lod, IL;

Inventors:

Eyal Peleg, Hedera, IL;

Tomer Valency, Shimshit, IL;

Ilan Barboi, Kfar Uriyya, IL;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2023.01); B64C 29/00 (2006.01); B64U 10/13 (2023.01); B64U 30/12 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/20 (2023.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64C 29/0033 (2013.01); B64U 10/13 (2023.01); B64U 30/12 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/20 (2023.01);
Abstract

According to at least one example a launch system is provided, including a carrier vehicle and at least one payload vehicle. The payload vehicle includes a payload propulsion system and aerodynamic lift surfaces designed for providing the payload vehicle with aerodynamic powered flight at a design subsonic cruise speed at a desired altitude. The carrier vehicle is configured for carrying the at least one payload vehicle at least up to the desired altitude, and further includes a solid rocket propulsion system for propelling the launch system to the desired altitude. The carrier vehicle is configured for providing a predetermined forward speed at the desired altitude, correlated to the design subsonic cruise speed. The carrier vehicle is configured for releasing the payload vehicle with respect to the carrier vehicle at the desired altitude and the predetermined forward speed. The design subsonic cruise speed is less than 0.7 Mach number, and, the desired altitude is greater than 3 km.


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