Image not available
Other industries
Satellite Rocket Separation Mechanism China Suppliers and Factory
Leading China factory and suppliers of high-precision satellite-rocket separation mechanisms. Featuring non-initiating explosive separating nuts for high stiffness and reliable locking, our systems ensure low-impact unlocking and stable separation for small satellites up to 100kg.
SupplierAstralink Science and Technology Co., Ltd.www.space-navi.com
Source categories
About this product
Product information from the supplier.
The Satellite-Rocket Separation Mechanism is a high-precision aerospace engineering solution designed to ensure the safe and accurate deployment of satellites from their launch vehicles. Engineered for extreme space environments, this critical component provides the necessary kinetic impulse and reliability required to transition a satellite from its launch configuration to its operational orbit.
Utilizing advanced materials and rigorous aerospace standards, our separation systems are optimized for various satellite loads ranging from 5kg to 80kg. By integrating precision-engineered unlocking mechanisms and controlled separation velocities, we minimize tip-off rates and maximize orbital injection accuracy for mission-critical satellite deployments.
Detailed Parameters
| Product Codes | CG-JG-SM-10 / 20 / 60 | Applicable Load | 5~15kg / 15~40kg / 40~80kg |
|---|---|---|---|
| Separation Velocity | 0.4~0.6m/s | Weight | 1.2kg / 1.8kg / 3.3kg |
| Main Body Envelopment | 220x220x81mm to 390x390x85mm | Temperature Range | -70~+70℃ |
| Angular Velocity | Optimized for Minimal Tip-off | Unlocking Impact | Low-Shock Design |
| Supply Cycle | 3 Months | Material Grade | Space-Level Alloy |
Key Advantages
Extreme Durability
Operating range from -70 to +70℃ ensures stability in the harshest vacuum and thermal environments.
Rapid Lead Time
Efficient supply chain management allows for a competitive 3-month delivery cycle.
Precision Velocity
Maintains a consistent separation velocity of 0.4~0.6m/s for precise orbital insertion.
Scalable Capacity
Three distinct models available to support payloads from small cubesats up to 80kg satellites.
Low Shock Impact
Engineered to reduce unlocking impact, protecting sensitive on-board satellite instruments.
Aerospace Certified
Strict adherence to aviation and space-level manufacturing standards for maximum reliability.
Product Gallery
Management Platforms
Payload Integration
Seamlessly integrate satellite loads based on weight specifications (5kg-80kg).
Dynamic Calibration
Precision adjustment of separation velocity to meet specific orbital requirements.
Thermal Monitoring
Advanced monitoring for stability across -70℃ to +70℃ temperature gradients.
Impact Analysis
Real-time simulation of unlocking impacts to safeguard sensitive electronics.
Component Tracking
Full traceability of space-level materials used in the separation mechanism.
Cycle Optimization
Streamlined manufacturing to ensure a consistent 3-month delivery window.
Investment Return Comparison
| Performance Metric | Standard Mechanism | Our Advanced Solution |
|---|---|---|
| Deployment Reliability | Moderate | Ultra-High (Space-Grade) |
| Temperature Tolerance | Limited Range | Extreme (-70℃ to +70℃) |
| Payload Versatility | Single-Load Fixed | Multi-Range (5kg - 80kg) |
| Shock Impact | High Residual Shock | Minimized Low-Impact |
| Production Lead Time | 6-12 Months | Fast-Track 3 Months |
Frequently Asked Questions
Q: What is the maximum satellite load supported by these mechanisms?
We offer three models (CG-JG-SM-10, 20, and 60) that support loads of 5-15kg, 15-40kg, and 40-80kg respectively.
Q: How does the mechanism handle extreme space temperatures?
Our mechanisms are designed with specialized alloys and lubricants that remain operational within a temperature range of -70℃ to +70℃.
Q: What is the typical separation velocity for these products?
The separation velocity is precisely maintained between 0.4m/s and 0.6m/s to ensure safe distance between the rocket and the satellite.
Q: Can the separation mechanism be customized for specific satellite dimensions?
Yes, we provide different envelopment sizes from 220mm to 390mm to match your satellite's physical architecture.
Q: What is the lead time for ordering a separation system?
Our current standard supply cycle is approximately 3 months from order confirmation to delivery.
Q: How is the "unlocking impact" managed to prevent satellite damage?
We use low-shock release mechanisms that minimize the mechanical impulse transmitted to the satellite during the separation event.
Ready to Optimize Your Satellite Deployment?
Contact UsMore from this supplier
Astralink Science and Technology Co., Ltd.
