Resources Contact Us Home
Passive lateral vibration isolation system for a spacecraft launch vehicle

Image Number 7 for United States Patent #6012680.

A lateral acceleration force isolator that forms a part of an attachment fitting for a payload, such as a spacecraft or satellite, and launch vehicle assembly. An upper portion of the isolator is designed to be attached to the payload and a lower portion is designed to be attached to a launch vehicle. Flexures are positioned in an array between the upper and lower portions to accommodate lateral displacement in the payload attachment fitting, thereby isolating lateral acceleration forces.

  Recently Added Patents
Soybean cultivar CL1013665
Semiconductor device with an amorphous semi-insulating layer, temperature sensor, and method of manufacturing a semiconductor device
Data security for dynamic random access memory using body bias to clear data at power-up
Semiconductor device including insulating layer of cubic system or tetragonal system
Low offset, fast response voltage controlled current source and controlling method thereof
Method for transmitting a signal from a transmitter to a receiver in a power line communication network, transmitter, receiver, power line communication modem and power line communication syst
Sensing device and electronic apparatus
  Randomly Featured Patents
Voltage converting I/O driver circuit
Interconnections for a semiconductor device and method for forming same
Hardware-accelerated high availability integrated networked storage system
High-pressure gas discharge lamp for a lighting device
Magnetic sheet, method for producing the magnetic sheet, antenna, and portable communication device
Inverted electrical submersible pump completion to maintain fluid segregation and ensure motor cooling in dual-stream well
PH-sensitive polymer containing sulfonamide and its synthesis method
Fiber optics channel selection device
Articular surface repair
Magnitude comparison circuit