Professional Services
Electronic & Energy
Integrated Information Processing Computer
Using COTS components with redundant system architecture to achieve high reliability, low cost, and highly integrated computer system. Integrates multiple functional modules including satellite management, attitude and orbit control, thermal control, propulsion control, AD acquisition, power secondary distribution, customizable according to user requirements.
Technical Specifications
Low Cost —— Utilizes COTS (Commercial Off-The-Shelf) technology,Reduces development costs and shortens development cycles.
High Reliability — Hardware fault-tolerant architecture design combined with software autonomous fault handling to enhance reliability.
High Integration — Integrates functions including satellite management, attitude and orbit control, propulsion control, AD acquisition, and thermal control.
Customized Services — Capable of customized design based on user structural and functional requirements.
Propulsion & Fluid
Pneumatic Pressure System
Application
Suitable for filling high-pressure containers, leak testing of fluid systems or valve pipelines, gas seal pressure testing of oilfield blowout preventers, etc. Applicable media: air, nitrogen, helium, hydrogen, oxygen (special models, maximum 35MPa) and other gases.
Product Features
High output pressure, small size and weight, low noise, pollution-free, flexible configuration
Structure & Material
Thermal Protection Materials
Carbon fiber reinforced phenolic thermal protection material
Carbon fiber reinforced phenolic thermal protection material uses low-density 3D rigid structure as reinforcement, filled with nano-insulating phenolic resin to form carbon fiber reinforced phenolic aerogel material. Features include low density, high strength, ablation resistance and high insulation, high temperature resistance, oxidation resistance, capable of withstanding high temperature and high pressure atmospheric scouring environment during first cosmic velocity re-entry. Can be used in aerospace, aviation and civilian fields.
Carbon fiber reinforced phenolic thermal protection material
Formed by compounding cork particles, resin matrix and fillers. Features include low density, low thermal conductivity, ablation resistance, good flexibility, easy construction and fitting on complex surfaces, wide availability, low-cost maintenance, short construction cycle. Widely used in thermal protection fields of rockets, missiles and other spacecraft.
Professional Simulation
Orbit Simulation
Capable of orbit and trajectory design simulation. Can complete design and review of spacecraft orbital flight trajectories and re-entry trajectories. Reasonably selects perturbation terms based on orbit type. Can simultaneously complete related analysis work including tracking arc segments, coverage, eclipse duration, lifespan, providing main parameters such as re-entry range, overload, heat flux, offering top-level input for spacecraft overall design.