10 results about "Space Shuttle" patented technology

A method for evaluating terrain uncertainty in flood warning and forecasting is provided. The method includes: S1, acquiring three types of digital elevation model (DEM) data from a shuttle radar topography mission (SRTM), an advanced spaceborne thermal emission and reflection radiometer (ASTER), and an advanced land observing satellite (ALOS); and preprocessing the three types of DEM data; S2, optimizing urban terrain characteristics; S3, constructing a multidimensional parameter space by using Latin hypercube sampling (LHS); S4, calculating flood hydrodynamics numerical value based on multidimensional sample points; and S5, constructing a global sensitivity analysis method frame suitable for urban terrain characteristics-related factors, where a Sobol quantitative method is used in the global sensitivity analysis method frame, and the Sobol quantitative method is used to evaluate uncertainties and sensitivity characteristics of multiple factors of terrain data based on a variance decomposition theory.

1. Name of the product in this design: Sightseeing vehicle (space shuttle). 2. Purpose of this design: This design is intended for sightseeing and tourism. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

1. The name of the design product: building blocks (space shuttle). 2. The use of the design product: building blocks. 3. The design features of the design product: in shape. 4. The picture or photo that best indicates the design features: perspective view.

The utility model relates to the technical field of model airplanes, and discloses a space shuttle model undercarriage mechanism which comprises two first shells, second fixing plates are fixedly connected to the left end and the right end of the front side of the first shell on the rear side, a self-locking mechanism is rotationally connected to the outer walls of the second fixing plates, and a third fixing plate is rotationally connected to the bottom end of the self-locking mechanism. A hatch cover is fixedly connected between the adjacent rear sides of the two third fixing plates, and a first fixing plate is fixedly connected to the middle of the front side of the first shell on the rear side. In the utility model, the motor is started to output power, the first rotary joint is driven to rotate through the transmission connecting rod, the wheels are driven to turn over to touch the ground, and after the transmission connecting rod is in place, the self-locking mechanism at the second rotary joint locks and prevents reverse movement, so that the transmission precision and the scene reduction degree are improved, the stable unfolding posture of the undercarriage is kept, and the cabin cover of the undercarriage is simultaneously opened in the process; and the process is ensured to be smooth and unobstructed, so that daily use requirements of operators are met.

Disclosed is a complex scene deformation monitoring and classifying method based on interferometric synthetic aperture radar (InSAR) and a deep learning self-attention model, including: generating a deformation interferogram by using an InSAR extraction technology combining persistent scatterer (PS) points and distributed scatter (DS) points and relying on a shuttle radar topography mission digital elevation model (SRTM DEM) image; constructing a Delaunay triangulation network and an annular zone, obtaining a time series deformation data of PS points and DS points through adaptive arc densification and omni-directional point expansion, and extracting settlement points on a bridge; decomposing a time series by an SAR-self-attention model, decomposing InSAR time series data into a trend component and a seasonal component, and interpreting and analyzing deformation of the sea-crossing bridge; and describing time series dynamics and a seasonal pattern by comparing a curve fitting method with a seasonal and trend decomposition method.

1. The name of the design product: eraser (time and space shuttle). 2. The use of the design product: for eraser. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view 1.

This utility model relates to the field of model aircraft technology and discloses an electric mechanism for the canopy of a space shuttle model. It includes a base plate, with L-shaped plates fixedly connected to the front and rear top sides of the base plate. An arc-shaped shell is fixedly connected between adjacent tops of two L-shaped plates. A bracket is fixedly connected to the inner center of each arc-shaped shell. A motor is fixedly connected between adjacent brackets. A worm gear is fixedly connected to the output end of the motor, and a worm wheel is meshed with the outer wall of the worm gear. In this utility model, the electric automated opening and closing of the canopy door is achieved by driving a worm gear transmission system and a hinge structure with a motor. Compared to traditional manual opening and closing methods, this greatly improves the convenience, efficiency, and reliability of the canopy door operation, providing a better opening and closing solution for related application scenarios. It also reduces manual operation costs and enhances the overall intelligence level of the equipment and the user experience.

The application discloses a tank suitable for a reusable carrier, relates to the field of reusable earth-to-space shuttles, and comprises a tank body and a partition plate assembly arranged in the tank body. The partition plate assembly comprises a passage communicating between two sides of the partition plate and a movable plate. Propellant can flow downward through the passage. When the propellant shakes upward, the propellant pushes the movable plate to move upward and closes the passage. The tank can adapt to flight overload. When propellant moves forward due to the overload, the movable plate moves forward to close the opening of the top plate, so that the propellant is closed at the bottom of the tank, the movement of the propellant to the front bottom of the tank is effectively inhibited, and the manufacturing scheme is simple and reliable and has high universality.

1. Name of the designed product: VR virtual experience device (space shuttle). 2. Use of the designed product: virtual environment matching device. 3. Design points of the designed product: in shape. 4. Picture or photo best indicating the design points: perspective view 1.