{"id":423577,"date":"2024-10-20T06:47:14","date_gmt":"2024-10-20T06:47:14","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bsi-pd-cen-clc-tr-17603-31-152021-2\/"},"modified":"2024-10-26T12:44:14","modified_gmt":"2024-10-26T12:44:14","slug":"bsi-pd-cen-clc-tr-17603-31-152021-2","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bsi-pd-cen-clc-tr-17603-31-152021-2\/","title":{"rendered":"BSI PD CEN\/CLC\/TR 17603-31-15:2021"},"content":{"rendered":"

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.<\/p>\n

The Thermal design handbook is published in 16 Parts<\/p>\n

TR 17603-31-01 Thermal design handbook \u2013 Part 1: View factors<\/p>\n

TR 17603-31-02 Thermal design handbook \u2013 Part 2: Holes, Grooves and Cavities<\/p>\n

TR 17603-31-03 Thermal design handbook \u2013 Part 3: Spacecraft Surface Temperature<\/p>\n

TR 17603-31-04 Thermal design handbook \u2013 Part 4: Conductive Heat Transfer<\/p>\n

TR 17603-31-05 Thermal design handbook \u2013 Part 5: Structural Materials: Metallic and Composite<\/p>\n

TR 17603-31-06 Thermal design handbook \u2013 Part 6: Thermal Control Surfaces<\/p>\n

TR 17603-31-07 Thermal design handbook \u2013 Part 7: Insulations<\/p>\n

TR 17603-31-08 Thermal design handbook \u2013 Part 8: Heat Pipes<\/p>\n

TR 17603-31-09 Thermal design handbook \u2013 Part 9: Radiators<\/p>\n

TR 17603-31-10 Thermal design handbook \u2013 Part 10: Phase \u2013 Change Capacitors<\/p>\n

TR 17603-31-11 Thermal design handbook \u2013 Part 11: Electrical Heating<\/p>\n

TR 17603-31-12 Thermal design handbook \u2013 Part 12: Louvers<\/p>\n

TR 17603-31-13 Thermal design handbook \u2013 Part 13: Fluid Loops<\/p>\n

TR 17603-31-14 Thermal design handbook \u2013 Part 14: Cryogenic Cooling<\/p>\n

TR 17603-31-15 Thermal design handbook \u2013 Part 15: Existing Satellites<\/p>\n

TR 17603-31-16 Thermal design handbook \u2013 Part 16: Thermal Protection System<\/p>\n

PDF Catalog<\/h4>\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n\n
PDF Pages<\/th>\nPDF Title<\/th>\n<\/tr>\n
2<\/td>\nundefined <\/td>\n<\/tr>\n
12<\/td>\n1 Scope <\/td>\n<\/tr>\n
13<\/td>\n2 References <\/td>\n<\/tr>\n
14<\/td>\n3 Terms, definitions and symbols
3.1 Terms and definitions
3.2 Abbreviated terms <\/td>\n<\/tr>\n
19<\/td>\n3.3 Symbols <\/td>\n<\/tr>\n
20<\/td>\n4 International ultraviolet explorer (IUE)
4.1 Mission
4.2 Main subsystems <\/td>\n<\/tr>\n
22<\/td>\n4.3 Main characteristics of the satellite <\/td>\n<\/tr>\n
23<\/td>\n4.4 Orbit <\/td>\n<\/tr>\n
24<\/td>\n4.5 Thermal design requirements <\/td>\n<\/tr>\n
26<\/td>\n4.6 Design tradeoffs
4.7 Thermal control of various components <\/td>\n<\/tr>\n
27<\/td>\n4.8 Estimated on orbit performance <\/td>\n<\/tr>\n
31<\/td>\n5 Orbital test satellite (OTS)
5.1 Mission
5.2 Main subsystems <\/td>\n<\/tr>\n
34<\/td>\n5.3 Main characteristics of the satellite <\/td>\n<\/tr>\n
37<\/td>\n5.4 Orbit
5.5 Thermal design requirements <\/td>\n<\/tr>\n
38<\/td>\n5.6 Design tradeoffs
5.7 Thermal control of various components <\/td>\n<\/tr>\n
44<\/td>\n5.8 Estimated on orbit performance
5.9 Measured in orbit performance <\/td>\n<\/tr>\n
51<\/td>\n6 Landsat D
6.1 Mission
6.2 Main subsystems <\/td>\n<\/tr>\n
52<\/td>\n6.3 Main characteristics of the satellite: <\/td>\n<\/tr>\n
53<\/td>\n6.4 Orbit
6.5 Thermal design requirements <\/td>\n<\/tr>\n
54<\/td>\n6.6 Design tradeoffs
6.7 Thermal control of various components <\/td>\n<\/tr>\n
56<\/td>\n6.8 Estimated on orbit performance <\/td>\n<\/tr>\n
58<\/td>\n6.9 Verification <\/td>\n<\/tr>\n
59<\/td>\n6.10 Measured on orbit performance <\/td>\n<\/tr>\n
60<\/td>\n7 Infrared astronomical satellite (IRAS)
7.1 Mission
7.2 Main subsystems <\/td>\n<\/tr>\n
62<\/td>\n7.3 Spacecraft main characteristics <\/td>\n<\/tr>\n
63<\/td>\n7.4 Orbit <\/td>\n<\/tr>\n
64<\/td>\n7.5 Thermal design requirements <\/td>\n<\/tr>\n
65<\/td>\n7.6 Design constraints <\/td>\n<\/tr>\n
66<\/td>\n7.7 Thermal control of various components <\/td>\n<\/tr>\n
69<\/td>\n7.8 Test of the spacecraft system <\/td>\n<\/tr>\n
70<\/td>\n7.9 Test of the superfluid Helium Dewar
7.9.1 General <\/td>\n<\/tr>\n
71<\/td>\n7.9.2 Test of the plug <\/td>\n<\/tr>\n
72<\/td>\n7.9.3 Prelaunch preparations <\/td>\n<\/tr>\n
73<\/td>\n7.10 On orbit performance of the spacecraft <\/td>\n<\/tr>\n
74<\/td>\n7.11 On orbit performance of the cryogenic system <\/td>\n<\/tr>\n
78<\/td>\n8 Satellite probatoire d\u2019observation de la terre (SPOT)
8.1 Mission
8.2 Main subsystems <\/td>\n<\/tr>\n
79<\/td>\n8.3 Main characteristics of the satellite <\/td>\n<\/tr>\n
82<\/td>\n8.4 Orbit
8.5 Thermal design requirements
8.5.1 Functional modes
8.5.2 Orbital constraints <\/td>\n<\/tr>\n
83<\/td>\n8.5.3 Limiting temperatures <\/td>\n<\/tr>\n
85<\/td>\n8.5.4 Thermal interfaces
8.6 Design tradeoffs <\/td>\n<\/tr>\n
86<\/td>\n8.7 Thermal control of various components
8.7.1 Platform <\/td>\n<\/tr>\n
87<\/td>\n8.7.1.1 Outer Elements
8.7.1.2 Inner Elements
8.7.1.3 Propulsion System
8.7.2 Batteries compartment <\/td>\n<\/tr>\n
89<\/td>\n8.7.3 High-resolution visible range instruments <\/td>\n<\/tr>\n
92<\/td>\n8.7.4 Payload telemetry system <\/td>\n<\/tr>\n
94<\/td>\n8.8 Estimated on-orbit performance
8.8.1 Platform <\/td>\n<\/tr>\n
95<\/td>\n8.8.2 Batteries compartment <\/td>\n<\/tr>\n
97<\/td>\n8.8.3 High-resolution visible range instrument
8.8.4 Payload telemetry system <\/td>\n<\/tr>\n
99<\/td>\n9 Olympus-1
9.1 Mission
9.2 Main subsystems <\/td>\n<\/tr>\n
104<\/td>\n9.3 Orbit
9.4 Thermal design requirements
9.5 Thermal control <\/td>\n<\/tr>\n
107<\/td>\n9.6 Thermal test of olympus-1 <\/td>\n<\/tr>\n
108<\/td>\n9.6.1 Thermal vacuum test <\/td>\n<\/tr>\n
111<\/td>\n9.6.2 Infrared test <\/td>\n<\/tr>\n
116<\/td>\n10 ERS-1
10.1 Mission <\/td>\n<\/tr>\n
117<\/td>\n10.2 Main subsystems <\/td>\n<\/tr>\n
121<\/td>\n10.3 Orbit
10.4 Thermal design requirements <\/td>\n<\/tr>\n
124<\/td>\n10.5 Thermal control <\/td>\n<\/tr>\n
128<\/td>\n10.6 Thermal tests
10.6.1 Thermal balance test of the engineering model <\/td>\n<\/tr>\n
134<\/td>\n10.6.2 Thermal vacuum test <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":"

Space Engineering. Thermal design handbook – Existing Satellites<\/b><\/p>\n\n\n\n\n
Published By<\/td>\nPublication Date<\/td>\nNumber of Pages<\/td>\n<\/tr>\n
BSI<\/b><\/a><\/td>\n2021<\/td>\n140<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n","protected":false},"featured_media":423584,"template":"","meta":{"rank_math_lock_modified_date":false,"ep_exclude_from_search":false},"product_cat":[2641],"product_tag":[],"class_list":{"0":"post-423577","1":"product","2":"type-product","3":"status-publish","4":"has-post-thumbnail","6":"product_cat-bsi","8":"first","9":"instock","10":"sold-individually","11":"shipping-taxable","12":"purchasable","13":"product-type-simple"},"_links":{"self":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product\/423577","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product"}],"about":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/types\/product"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media\/423584"}],"wp:attachment":[{"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/media?parent=423577"}],"wp:term":[{"taxonomy":"product_cat","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_cat?post=423577"},{"taxonomy":"product_tag","embeddable":true,"href":"https:\/\/pdfstandards.shop\/wp-json\/wp\/v2\/product_tag?post=423577"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}