🔥🔥 Don’t Miss Out on Our End of Autumn Sale. If you have any questions, feel free to click the bottom right corner to contact our customer service..

Concat us[email protected]
Shopping Cart

No products in the cart.

🔍
BS ISO 17401:2023

BS ISO 17401:2023

$142.49

Space systems. Spacecraft interface requirements document for launch vehicle services

Published By Publication Date Number of Pages
BSI 2023 32
PDF Format Searchable Printable Preview Now
Guaranteed Safe Checkout
Category:

If you have any questions, feel free to reach out to our online customer service team by clicking on the bottom right corner. We’re here to assist you 24/7.
Email:[email protected]

PDF Catalog

PDF Pages PDF Title
2 National foreword
7 Foreword
8 Introduction
9 1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
3.1 Terms and definitions
3.2 Abbreviated terms
10 4 Spacecraft mission description
4.1 Mission description
4.2 SC description (optional)
5 Mechanical interfaces
5.1 Mechanical configuration
5.2 SC fundamental frequencies
11 5.3 Usable volume
5.4 Spacecraft (or SC adapter) mechanical interface
5.5 Connectors and microswitches (SC side of the interface)
12 5.6 Purges and fluid connection interface
5.7 Encapsulated spacecraft access
6 Electrical interfaces
6.1 Umbilical wiring diagram
6.2 Umbilical connectors
13 6.3 Umbilical wiring links (for each connector pin)
6.4 Electrical commands dedicated to spacecraft
6.4.1 Pyrotechnic commands
14 6.4.2 Dry loop commands
6.4.3 Electrical commands
15 6.5 Separation status transmission
6.6 SC in-flight telemetry
6.7 Power supply required from LV
6.8 Earth potential continuity
16 7 Radio-frequency and electromagnetic interface
7.1 Characteristics of radio-electrical systems
17 7.2 RF telemetry and command link
7.2.1 SC RF-link definition for ground operations
7.2.2 SC antenna coordinates
7.2.3 RF-link implementation
7.2.4 RF-link budget
18 7.2.5 Base band signal characteristics
19 8 Spacecraft mission characteristics
8.1 SC input data for mission analyses
8.1.1 Mass and inertia characteristics
8.1.2 Sloshing masses (pendulum-type)
20 8.1.3 SC mission constraints (when applicable)
8.2 SC orbit parameters (with tolerances)
21 8.3 Launch window
8.3.1 Launch window constraints (when applicable)
8.3.2 Preferred window
8.4 SC pointing and separation
9 Environment requirements
9.1 General
9.2 Mechanical environment
22 9.3 Thermal environment
9.4 Static pressure
23 9.5 Contamination and cleanliness control
9.6 Radio frequency and electromagnetic environment
9.7 Environment monitoring
9.8 Exposure to sun
10 SC Development and test programme
10.1 Mechanical environment qualification tests
24 10.2 LV/SC compatibility tests
11 Launch range operations: facilities and support requirements
11.1 General logistics requirements
11.1.1 General
11.1.2 SC container and ground support equipment physical envelopes
25 11.1.3 Material handling equipment
11.1.4 Electrical power for SC and ground station
11.1.5 Umbilical lines and ground lines
11.1.6 Gas and fluid lines
26 11.1.7 Clean room
11.1.8 Environmental controls for SC and ground station
11.1.9 Clothing (safety and cleanroom)
11.1.10 Area
27 11.1.11 Storage (non-hazardous items)
11.1.12 SC pre-launch activities calendar
11.1.13 Special technical support equipment
11.1.14 Other
28 11.2 Specific requirements for solid propellant motor facilities (Y/N, to specify)
11.2.1 Solid propellant motor storage
11.2.2 Pyrotechnics storage
11.3 Specific requirements for X-ray facilities
11.4 Specific requirements for hazardous operations facilities
11.4.1 Gases
29 11.4.2 Liquid propellant
11.4.3 SC purge requirements
11.4.4 SC fluid requirements
11.5 Payload handling and transport requirements
30 11.6 Communication requirements
11.7 General range services
11.8 Safety requirements
12 Other requirements
31 Bibliography

Related products

BS ISO 17401:2023
$142.49