Sign In |Help & Support
ALL SECTORS
  • ALL SECTORS
  • GB(National Standard)
  • CB(Shipping)
  • CECS(Engineering Construction)
  • CJ(Urban Construction)
  • CY(News and Publication)
  • DB(Provincial Standard)
  • DL(Electricity & Power)
  • DZ(Geology & Mineralogy)
  • FZ(Spinning & Textile)
  • GA(Public Security)
  • HB(Aviation)
  • HG(Chemical Industry)
  • HJ(Environmental Protection)
  • JB(Machinery)
  • JC(Building Materials)
  • JG(Building & Construction)
  • JJ(Metering)
  • JT(Highway & Transportation)
  • LY(Forestry)
  • MT(Coal)
  • NB(Energy)
  • NY(Agriculture)
  • QB(Light Industry)
  • QC(Automobile & Vehicle)
  • QJ(Aerospace)
  • SH(Petrochemical)
  • SJ(Electronics)
  • SL(Water Resources)
  • SN(Commodity Inspection)
  • SY(Oil & Gas)
  • TB(Railway & Train)
  • YB(Ferrous Metallurgy)
  • YC(Tobacco)
  • YD(Telecommunication)
  • YY(Medical Device)
Database: 365,228(8 Aug 2026)
test method method satellite thermal control coatings test method test method 2502.3-2015 standard name test method normal emissivity method nuts scopethis standard specifies displayed characters membrane test
GJB 2502.3-2015 in English

GJB 2502.3-2015 in English

VALID

Test method for thermal control coatings of spacecraft. Part 3: Measurement of emissivity

  • Issued on:2015-12-19
  • Implemented on:2016-03-01
  • File Format:PDF
  • Delivery:Via email within 1~3 business days
Price(USD): $200.00
$194.00
Standard No: GJB 2502.3-2015
Document status: VALID
Title in English: Test method for thermal control coatings of spacecraft. Part 3: Measurement of emissivity
Title in Chinese: 航天器热控涂层试验方法 第3部分:发射率测试
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 1~3 business days
Issued on: 2015-12-19
Implemented on: 2016-03-01
Professional Classification: GJB-Military
Related Keywords: test method method
satellite thermal control coatings test method
test method
2502.3-2015 standard name test method
normal emissivity method
Related Topics: Aerodynamic test of spacecraft thermal control coating
Thermal Control Coating
emissivity
gjb 2015
Thermal control
Spacecraft
hemispherical reflectance
High emissivity
hemispherical reflectance
Spacecraft heat pipe test method
Dual-band emissivity tester test
Spacecraft thermal control coating test methods
Chinese Spaceflight


Introduction

Standard Evolution and Framework

Comparison Dimensions GJB 2502-1995 GJB 2502.3-2015
Standard Name Test Method for Satellite Thermal Control Coatings Test Method for Spacecraft Thermal Control Coatings Part 3
Test Method Method 310/330/350/370 Method 2011/2021/2031/2041
New Technologies - Radiometer Method (Method 2031)

Analysis of Core Test Methods

1. Steady-state Calorimeter Method (Method 2011)

The hemispherical emissivity is calculated by the principle of electric power compensation using a vacuum cold wall device with a test range of 0.03-0.98 and an accuracy of ±0.01. Key equipment includes:

  • Main/auxiliary heating system
  • Liquid nitrogen constant temperature heat sink (emissivity ≥ 0.90)
  • Standard resistor with accuracy of 0.05%

2. Normal emissivity method (Method 2021)

Based on the blackbody cavity comparison principle, using planar thermopile detector, the test range is 0.04-0.98, and the accuracy is ±0.015.

  • Metal substrate thickness ≤ 1.8mm
  • 40mm×40mm standard size
  • Surface roughness Ra ≤ 0.8μm

Implementation suggestions

Method selection guide

Application scenarios Recommended methods Advantages
Precise laboratory measurement Steady-state calorimeter method Full-band measurement
On-site rapid detection Radiometer method Portable and efficient

Key points of quality control

  1. Regularly calibrate the blackbody cavity (emissivity ≥ 0.90)
  2. Maintain vacuum degree ≤ 1.0×10-3Pa
  3. Sample temperature fluctuation control ≤ ± 0.1℃

Sample only — not a preview of GJB 2502.3-2015
Page: 1 / 0
100%

Loading PDF document...

Error loading PDF. Please make sure the file is valid and try again.

We also recommend