Blue origin llc (20240092508). STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS simplified abstract
Contents
- 1 STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Unanswered Questions
- 1.11 Original Abstract Submitted
STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS
Organization Name
Inventor(s)
Shane Draney of Maple Valley WA (US)
Robert E. Mcmullen of Redmond WA (US)
STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240092508 titled 'STUD-PROPELLING MECHANISMS FOR SECURING A LAUNCH VEHICLE TO A LANDING PLATFORM, AND ASSOCIATED SYSTEMS AND METHODS
Simplified Explanation
The patent application describes mechanisms for securing a launch vehicle to a landing platform using a fastening mechanism carried by a landing support element. The mechanism includes a barrel structure for propelling a stud that binds in the landing surface to fasten the landing support element.
- The fastening mechanism is carried by a landing support element of the launch vehicle.
- The mechanism includes a barrel structure for propelling a stud.
- An interference portion receives the stud upon activation of an energetic material.
- The stud binds in the interference portion and the landing surface to fasten the landing support element.
Potential Applications
The technology can be applied in the aerospace industry for securing launch vehicles to landing platforms.
Problems Solved
This technology solves the problem of securely fastening a launch vehicle to a landing platform.
Benefits
The benefits of this technology include improved safety and stability during the landing process of launch vehicles.
Potential Commercial Applications
The technology can be commercialized for use in space exploration missions for securing rockets during landing.
Possible Prior Art
There may be prior art related to mechanisms for securing objects to surfaces using fastening mechanisms, but specific examples are not provided in the abstract.
Unanswered Questions
How does the energetic material activate to propel the stud?
The abstract does not provide details on how the energetic material activates to propel the stud. Further information on this process would be helpful.
What materials are used in the construction of the fastening mechanism?
The abstract does not mention the specific materials used in the construction of the fastening mechanism. Understanding the materials involved could provide insights into the durability and effectiveness of the system.
Original Abstract Submitted
stud-propelling mechanisms for securing a launch vehicle to a landing platform, and associated systems and methods, are disclosed. a representative system includes a fastening mechanism carried by a landing support element of a portion of a launch vehicle, the mechanism configured to fasten the landing support element to the landing surface when the launch vehicle portion is on the landing surface. the fastening mechanism can include a barrel structure for propelling a stud and an interference portion positioned to receive the stud upon activation of an energetic material that propels the stud. the stud can bind in the interference portion and in the landing surface to fasten the landing support element to the landing surface. a representative method includes automatically fastening a portion of a launch vehicle to a landing surface using a stud carried by the portion of the launch vehicle.
