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BSI PD CEN/CLC/TR 17603-31-15:2021

BSI PD CEN/CLC/TR 17603-31-15:2021

$215.11

Space Engineering. Thermal design handbook – Existing Satellites

Published By Publication Date Number of Pages
BSI 2021 140
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In this Part 15, existing satellites are described and examined from a thermal control and design view. The thermal control requirements are given and an assessment is made of the thermal control systems used against performance for each satellite.

The Thermal design handbook is published in 16 Parts

TR 17603-31-01 Thermal design handbook – Part 1: View factors

TR 17603-31-02 Thermal design handbook – Part 2: Holes, Grooves and Cavities

TR 17603-31-03 Thermal design handbook – Part 3: Spacecraft Surface Temperature

TR 17603-31-04 Thermal design handbook – Part 4: Conductive Heat Transfer

TR 17603-31-05 Thermal design handbook – Part 5: Structural Materials: Metallic and Composite

TR 17603-31-06 Thermal design handbook – Part 6: Thermal Control Surfaces

TR 17603-31-07 Thermal design handbook – Part 7: Insulations

TR 17603-31-08 Thermal design handbook – Part 8: Heat Pipes

TR 17603-31-09 Thermal design handbook – Part 9: Radiators

TR 17603-31-10 Thermal design handbook – Part 10: Phase – Change Capacitors

TR 17603-31-11 Thermal design handbook – Part 11: Electrical Heating

TR 17603-31-12 Thermal design handbook – Part 12: Louvers

TR 17603-31-13 Thermal design handbook – Part 13: Fluid Loops

TR 17603-31-14 Thermal design handbook – Part 14: Cryogenic Cooling

TR 17603-31-15 Thermal design handbook – Part 15: Existing Satellites

TR 17603-31-16 Thermal design handbook – Part 16: Thermal Protection System

PDF Catalog

PDF Pages PDF Title
2 undefined
12 1 Scope
13 2 References
14 3 Terms, definitions and symbols
3.1 Terms and definitions
3.2 Abbreviated terms
19 3.3 Symbols
20 4 International ultraviolet explorer (IUE)
4.1 Mission
4.2 Main subsystems
22 4.3 Main characteristics of the satellite
23 4.4 Orbit
24 4.5 Thermal design requirements
26 4.6 Design tradeoffs
4.7 Thermal control of various components
27 4.8 Estimated on orbit performance
31 5 Orbital test satellite (OTS)
5.1 Mission
5.2 Main subsystems
34 5.3 Main characteristics of the satellite
37 5.4 Orbit
5.5 Thermal design requirements
38 5.6 Design tradeoffs
5.7 Thermal control of various components
44 5.8 Estimated on orbit performance
5.9 Measured in orbit performance
51 6 Landsat D
6.1 Mission
6.2 Main subsystems
52 6.3 Main characteristics of the satellite:
53 6.4 Orbit
6.5 Thermal design requirements
54 6.6 Design tradeoffs
6.7 Thermal control of various components
56 6.8 Estimated on orbit performance
58 6.9 Verification
59 6.10 Measured on orbit performance
60 7 Infrared astronomical satellite (IRAS)
7.1 Mission
7.2 Main subsystems
62 7.3 Spacecraft main characteristics
63 7.4 Orbit
64 7.5 Thermal design requirements
65 7.6 Design constraints
66 7.7 Thermal control of various components
69 7.8 Test of the spacecraft system
70 7.9 Test of the superfluid Helium Dewar
7.9.1 General
71 7.9.2 Test of the plug
72 7.9.3 Prelaunch preparations
73 7.10 On orbit performance of the spacecraft
74 7.11 On orbit performance of the cryogenic system
78 8 Satellite probatoire d’observation de la terre (SPOT)
8.1 Mission
8.2 Main subsystems
79 8.3 Main characteristics of the satellite
82 8.4 Orbit
8.5 Thermal design requirements
8.5.1 Functional modes
8.5.2 Orbital constraints
83 8.5.3 Limiting temperatures
85 8.5.4 Thermal interfaces
8.6 Design tradeoffs
86 8.7 Thermal control of various components
8.7.1 Platform
87 8.7.1.1 Outer Elements
8.7.1.2 Inner Elements
8.7.1.3 Propulsion System
8.7.2 Batteries compartment
89 8.7.3 High-resolution visible range instruments
92 8.7.4 Payload telemetry system
94 8.8 Estimated on-orbit performance
8.8.1 Platform
95 8.8.2 Batteries compartment
97 8.8.3 High-resolution visible range instrument
8.8.4 Payload telemetry system
99 9 Olympus-1
9.1 Mission
9.2 Main subsystems
104 9.3 Orbit
9.4 Thermal design requirements
9.5 Thermal control
107 9.6 Thermal test of olympus-1
108 9.6.1 Thermal vacuum test
111 9.6.2 Infrared test
116 10 ERS-1
10.1 Mission
117 10.2 Main subsystems
121 10.3 Orbit
10.4 Thermal design requirements
124 10.5 Thermal control
128 10.6 Thermal tests
10.6.1 Thermal balance test of the engineering model
134 10.6.2 Thermal vacuum test

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