YDNFoam™ Ultra-Light Melamine Foam — Thermal Insulation for Spacecraft Battery Compartments
1. Background: Managing Extreme Temperature in Aerospace Power Systems
YDNFoam™ Ultra-Light Melamine Foam — Thermal Insulation for Spacecraft Battery Compartments
1. Background: Managing Extreme Temperature in Aerospace Power Systems
In spacecraft, battery compartments are mission-critical components responsible for power supply and stability. During orbital operation and re-entry, these compartments face extreme thermal swings from –150 °C to +180 °C, vacuum, vibration, and radiation.
Uncontrolled heat transfer may cause:
· Thermal runaway and battery degradation
· Capacity loss and reduced lifespan
· Increased structure weight due to redundant safety margins
Hence, aerospace power modules demand lightweight, intrinsically flame-retardant, and wide-temperature-stable insulation materials — such as YDNFoam™.
2. Material Properties: Aerospace-Grade Advantages of YDNFoam™
YDNFoam™ ultra-light melamine foam (density ≈ 4 kg/m³) features nano-scale open-cell porosity and nitrogen-rich molecular stability, ensuring outstanding thermal and mechanical integrity in vacuum or cryogenic conditions.

Property
Typical Value
Functional Significance
Thermal Conductivity (λ)
≤ 0.032 W/m·K
Maintains insulation under vacuum and extreme cold
Operating Temperature
–200 °C — +240 °C
Covers entire spacecraft mission range
Sound Absorption (NRC)
≥ 0.85
Damps vibration and acoustic noise
Flame Retardancy
UL 94 V-0 / EN 45545–2 R1 HL3
Intrinsically flame-retardant, no additives required
Density
4 kg/m³
Ultra-lightweight, reduces payload mass
Chemical Resistance
Stable to electrolytes, acids, and ethanol
Ensures long-term stability
3. Structural Integration: Three-Layer Thermal Barrier Design
YDNFoam™ can be configured into a multi-layer insulation system for battery bays:
1. Inner Conductive Isolation Layer — Laminated with aluminum foil or polyimide film to enhance heat reflection.
2. Middle Buffer Layer — Provides vibration damping and shock absorption.
3. Outer Radiative Shield Layer — Uses metallized PET or aerogel composites for radiation protection.
A composite structure of ≈ 300 g/m² total weight maintains a temperature differential of –120 °C ~ +150 °C, ideal for CubeSats, deep-space probes, and reusable rocket compartments.
4. Typical Aerospace Applications
· Satellite battery bays
· Reusable rocket power compartments
· Deep-space probe energy modules
· Electric-propulsion bay thermal shields
5. Sustainability and Integration
· 100% nitrogen-based polymer, halogen-free and non-toxic.
· Compatible with thermoforming (YDNFoam-TG) for complex geometries.
· Easily integrated with aerogels, aramid honeycombs, or carbon composites.
6. Conclusion
YDNFoam™ provides a lightweight, flame-safe, and wide-temperature insulation solution for next-generation aerospace systems. With intrinsic stability from –200 °C to +240 °C and λ ≤ 0.032 W/m·K, it ensures energy reliability, reduced structural weight, and superior safety for spacecraft battery modules and power systems.
Contact YDNFoam™
YDNFoam | A Division of YDN Group Address: №2088, Jiuliting Avenue, Caoqiao Street, Pinghu City, Zhejiang Province, China Email: sales@ydnfoam.com Website: www.ydnfoam.com Phone / WeChat: +86–135–4070–2776
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