by selecting the beam type (i.e., I-beam, C-beam, T-beam) or panel type (i.e., hat-stiffened, honeycomb sandwich, orthogrid) and sets the upper and lower limits on geometric parameters (i.e., beam height, panel height, facesheet thickness, web spacing) and the number of permutations to consider for each geometric parameter. In addition, the
Project: Composite Structures • Objective: Develop new analysis-based buckling knockdown factors (KDFs) for composite launch-vehicle structures • Scope – Sandwich-composite cylinders – Acreage designs – Axial compression • Approach – Analysis-based knockdown factor development and validation • Develop and assess various ...
The paper describes the present design configuration for the Upper Liquid Propulsion Module (ULPM), the Lower Liquid Propulsion Module (LLPM) and the metallic skirts of the equipped solid rocket motor, together with the engineering, technology development and industrialization activities in order to deliver the products with the required perform...
Design of a typical aerospace interstage structure using orthogrid ...
May 17, 2023 · In this study, an interstage cylindrical shell structure of a Launch Vehicle is designed with isogrid and orthogrid configurations, which are integral-rib-stiffened-skin configurations to have mass-optimised aerospace structures.
Structural Design and Fabrication of a Rocket - CORE
Our senior project will focus specifically on the structure of the rocket. This includes the rocket body, and securing any subsystems. The motor, electronics bay, and recovery system are example of components which will need to be mounted. The project consists of two parts.
This structure performs several functions including primary launch vehicle load carrying, separation of the corresponding interior MPCV and DCSS environments through a spherical cap diaphragm, cable interface panels, access panels, and attachment interfaces for electrical cable wiring harness to span the ...
Study on panel flutter considering unsteady deceleration and …
2 days ago · Thin-walled elastic structures, which are frequently applied on reusable rocket bodies, can experience panel flutter issues easily under unsteady aerodynamic loads. After separation of the ascent stage or during the recovery stage, the first stage of the rocket may undergo a deceleration period in the transonic region.
Progress in Lightweight Design Methods for Large-Size Panel Structures ...
Jul 26, 2023 · Compared with the semi-monocoque shell structure, the panel structure greatly improves the load-bearing efficiency, fatigue resistance and reliability, effectively reduces the structural quality, and has the advantages of less parts, short process cycle, high …
(PDF) Design Optimization of an Isogrid or Orthogrid Tank for …
May 7, 2021 · Isogrid structures are commonly used for launch vehicles as load-bearing structures and/or tanks to hold fuel, compressed gases, etc. By using an isogrid tank (isotank) as a primary structural...
Jul 24, 2023 · Flat fixed stabilizing structures extending from the body of a rocket that give stability in flight. There are four common fin shapes: Each fin has several features used to characterize its design & performance: • Tip chord (c. t) • Root chord (c. r) • Span (b) • Leading Edge (LE) • Trailing Edge (TE) • Aspect ratio (AR) Hardware ...