Patents by Inventor John Zaniel Maccagnano
John Zaniel Maccagnano has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Publication number: 20240140583Abstract: The system can include: a vehicle 100 and a stabilizer 200. However, the system can additionally or alternatively include any other suitable set of components. The system functions to facilitate vehicular transport (e.g., via a cabin). Additionally, the system can provide impact attenuation and/or mitigate rebound of the vehicle during a water landing. Additionally or alternatively, the system can function to provide aquatic stabilization of the vehicle and/or cabin thereof. However, the system 100 can provide any other suitable functionalities.Type: ApplicationFiled: January 10, 2024Publication date: May 2, 2024Applicant: Space Perspective Inc.Inventors: Royce Fernandes, John Zaniel Maccagnano, Taber MacCallum, Ryon Warren, Daniel James Window, Rodger Farley
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Publication number: 20240140621Abstract: The cabin conditioning system can include a cabin air loop, a refrigerant loop, and a set of thermal rejection components. The system can optionally include a phase-change fluid loop. However, the cabin conditioning system can additionally or alternatively include any other suitable set of components. The cabin conditioning system functions to condition a cabin interior (and/or an air volume therein) of a vehicle, such as an atmospheric and/or space-flight capsule. Additionally or alternatively, the system can function to reject heat from the vehicle interior and/or vehicle power systems (e.g., avionics components thereof). Additionally or alternatively, the system can function to maintain the humidity of air within the cabin interior. However, the cabin conditioning system can include any other suitable components.Type: ApplicationFiled: January 10, 2024Publication date: May 2, 2024Applicant: Space Perspective Inc.Inventors: John Straus, Taber MacCallum, Hector Santiago, Tasneem Rashid, John Zaniel Maccagnano
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Patent number: 11945607Abstract: The cabin conditioning system can include a cabin air loop, a refrigerant loop, and a set of thermal rejection components. The system can optionally include a phase-change fluid loop. However, the cabin conditioning system can additionally or alternatively include any other suitable set of components. The cabin conditioning system functions to condition a cabin interior (and/or an air volume therein) of a vehicle, such as an atmospheric and/or space-flight capsule. Additionally or alternatively, the system can function to reject heat from the vehicle interior and/or vehicle power systems (e.g., avionics components thereof). Additionally or alternatively, the system can function to maintain the humidity of air within the cabin interior. However, the cabin conditioning system can include any other suitable components.Type: GrantFiled: February 9, 2023Date of Patent: April 2, 2024Assignee: Space Perspective Inc.Inventors: John Straus, Taber MacCallum, Hector Santiago, Tasneem Rashid, John Zaniel Maccagnano
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Patent number: 11904998Abstract: The system can include: a vehicle 100 and a stabilizer 200. However, the system can additionally or alternatively include any other suitable set of components. The system functions to facilitate vehicular transport (e.g., via a cabin). Additionally, the system can provide impact attenuation and/or mitigate rebound of the vehicle during a water landing. Additionally or alternatively, the system can function to provide aquatic stabilization of the vehicle and/or cabin thereof. However, the system 100 can provide any other suitable functionalities.Type: GrantFiled: July 19, 2023Date of Patent: February 20, 2024Assignee: Space Perspective Inc.Inventors: Royce Fernandes, John Zaniel Maccagnano, Taber MacCallum, Ryon Warren, Daniel James Window, Rodger Farley
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Publication number: 20240025529Abstract: The system can include: a vehicle 100 and a stabilizer 200. However, the system can additionally or alternatively include any other suitable set of components. The system functions to facilitate vehicular transport (e.g., via a cabin). Additionally, the system can provide impact attenuation and/or mitigate rebound of the vehicle during a water landing. Additionally or alternatively, the system can function to provide aquatic stabilization of the vehicle and/or cabin thereof. However, the system 100 can provide any other suitable functionalities.Type: ApplicationFiled: July 19, 2023Publication date: January 25, 2024Inventors: Royce Fernandes, John Zaniel Maccagnano, Taber MacCallum, Ryon Warren, Daniel James Window, Rodger Farley
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Publication number: 20230303270Abstract: The cabin conditioning system can include a cabin air loop, a refrigerant loop, and a set of thermal rejection components. The system can optionally include a phase-change fluid loop. However, the cabin conditioning system can additionally or alternatively include any other suitable set of components. The cabin conditioning system functions to condition a cabin interior (and/or an air volume therein) of a vehicle, such as an atmospheric and/or space-flight capsule. Additionally or alternatively, the system can function to reject heat from the vehicle interior and/or vehicle power systems (e.g., avionics components thereof). Additionally or alternatively, the system can function to maintain the humidity of air within the cabin interior. However, the cabin conditioning system can include any other suitable components.Type: ApplicationFiled: February 9, 2023Publication date: September 28, 2023Inventors: John Straus, Taber MacCallum, Hector Santiago, Tasneem Rashid, John Zaniel Maccagnano
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Publication number: 20230159173Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: ApplicationFiled: January 6, 2023Publication date: May 25, 2023Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Patent number: 11613364Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: GrantFiled: October 1, 2020Date of Patent: March 28, 2023Assignee: World View Enterprises Inc.Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Publication number: 20210122479Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: ApplicationFiled: October 1, 2020Publication date: April 29, 2021Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Patent number: 10829229Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: GrantFiled: June 7, 2017Date of Patent: November 10, 2020Assignee: World View Enterprises Inc.Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Patent number: 9962798Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: GrantFiled: July 27, 2016Date of Patent: May 8, 2018Assignee: Paragon Space Development CorporationInventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano
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Publication number: 20170349291Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: ApplicationFiled: June 7, 2017Publication date: December 7, 2017Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Patent number: 9694910Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: GrantFiled: February 24, 2014Date of Patent: July 4, 2017Assignee: World View Enterprises Inc.Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus, Jared Leidich, Daniel Pieter Jacobus Blignaut
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Publication number: 20160332268Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: ApplicationFiled: July 27, 2016Publication date: November 17, 2016Inventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano
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Patent number: 9429371Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: GrantFiled: June 22, 2015Date of Patent: August 30, 2016Assignee: Paragon Space Development CorporationInventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano
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Publication number: 20150285568Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: ApplicationFiled: June 22, 2015Publication date: October 8, 2015Inventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano
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Publication number: 20150284065Abstract: A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery.Type: ApplicationFiled: February 24, 2014Publication date: October 8, 2015Inventors: Taber K. MacCallum, Jacob H. Dang, Robert Alan Eustace, John Zaniel Maccagnano, Julian R. Nott, Sebastian A. Padilla, Sreenivasan Shankarnarayan, John Straus
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Patent number: 9091489Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: GrantFiled: May 13, 2011Date of Patent: July 28, 2015Assignee: PARAGON SPACE DEVELOPMENT CORPORATIONInventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano
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Publication number: 20110277959Abstract: A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.Type: ApplicationFiled: May 13, 2011Publication date: November 17, 2011Applicant: PARAGON SPACE DEVELOPMENT CORPORATIONInventors: Thomas William Morin, Taber K. MacCallum, Norman Jacob Hahn, John Zaniel Maccagnano