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GB/T 47459-2026Communication specification for the payload network of a space station (English PDF)

空间站载荷网通信规范

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Issued by

SAMR; SAC

Level / Type

National · Recommended

Issue date

April 30, 2026

Implementation date

November 1, 2026

Scope

GB/T 47459-2026 is the English-translated version of 空间站载荷网通信规范.

GB/T 47459-2026 is the Chinese national specification for the network that carries payload data aboard a space station.

It describes the architecture - the payload networks of the Tianhe, Wentian and Mengtian modules joined by 10 Gigabit fibre into one network, with backbone switches, access switches, a network manager and in-cabin and extravehicular wireless transceivers - and then fixes the protocols a terminal must follow at each layer: 100Base-TX, 1000Base-LX and 10GBase-LR per IEEE 802.3u, 802.3z and 802.3ae, IEEE 802.11a/n/ac/ax for the 5.2 GHz and 5.8 GHz wireless LAN, MAC frames without the LLC sublayer, IP, ARP and ICMP per RFC 791, 826 and 792, UDP and TCP, and SNMP, SNTP and FTP or TFTP above them.

It applies to the design and testing of payload network terminals. Issued on 30 April 2026, it has applied since 1 November 2026.

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Document preview — GB/T 47459-2026

National Standard of the People's Republic of China

ICS
35.020
Classification
L 78

Issued by: State Administration for Market Regulation; Standardization Administration of the PRC

Contents

  • 1 Scope
  • 4 Load Net Architecture
  • 5 Network Protocol Requirements
  • 6 Other communication requirements
  • 7 Test Requirements

1 Scope

This document specifies the space station payload network architecture, network protocol requirements, other communication requirements, and testing requirements.

This document applies to the design and testing of network terminals for space station payload networks (including wired Ethernet and wireless LAN).

4 Load Net Architecture

4.1 The Tianhe core module, Wentian experimental module, and Mengtian experimental module of the space station are all equipped with payload networks. A schematic diagram of the single-module payload network interface is shown in Figure 1. The lotus network architecture meets the following requirements.

a) In the combined configuration, the payload networks of each module are interconnected via 10 Gigabit fiber optic cables to form a unified network, providing on-orbit high-speed connectivity for network terminals.

Services include high-speed data transmission, high-speed data transmission between air and ground, and network management. The SSID of the wireless network inside and outside the cabin is the same.

b) The space station payload network mainly includes backbone switches, access switches, network manager, intravehicular radio transceivers, and extravehicular radio transceivers.

Products such as transceiver equipment. The quantity of access switches, in-cabin wireless transceiver equipment, and external wireless transceiver equipment in each cabin will be determined based on the actual situation in each cabin. The scale of the test load is determined.

4.2 The payload network provides network terminals with the following interface types. wired Ethernet interface and wireless LAN interface.

a) Wired Ethernet interface.

1) 10 Gigabit fiber optic interface;

2) Gigabit fiber optic interface;

3) 100M Ethernet interface.

b) Wireless LAN interface. 5.2GHz and 5.8GHz wireless LAN interfaces.

4.3 The relationship between the interface types provided by the payload network to the network end and the network protocol is shown in Table 1.

5 Network Protocol Requirements

5.1 Physical Layer

5.1.1 The physical layer protocol of the space station payload network shall meet the following requirements.

a) When connecting to a 100Mbps Ethernet interface, the physical layer protocol of the network terminal should comply with the 100Base-TX specification in IEEE std802.3u;

It should support an automatic data rate negotiation mechanism, be backward compatible, and the compatible interface should conform to IEEE std802.3u. The provisions of 10BASE-T.

b) When connecting to a gigabit fiber optic interface.

1) The physical layer protocol of the network terminal should conform to the 1000Base-LX specification in IEEE std802.3z;

2) The load network switch adopts full-duplex mode, the single-mode wavelength should be 1310nm±20nm, and the average optical power should be considerable.

The saturation optical power should be no less than 1 dBm and the receiver sensitivity should be no greater than -2 dBm. -16dBm;

3) The optical communication performance of the network terminal should be matched with that of the load network switch.

c) When connecting to a 10 Gigabit fiber optic interface.

1) The physical layer protocol of the network terminal should comply with the 10GB ase-LR specification in IEEE std 802.3ae;

2) The load network switch should adopt full-duplex mode, the single-mode wavelength should be 1310nm±20nm, and the average optical power should be not less.

The saturation optical power should be no less than -2dBm and the receiver sensitivity should be no greater than -5dBm. -19dBm;

3) The optical communication performance of the network terminal should be matched with that of the load network switch.

d) When accessing a wireless LAN, the physical layer protocol of the network terminal should conform to at least one of IEEE std 802.11a/n/ac/ax.

The types have center frequencies ranging from 5.18 GHz to 5.32 GHz and from 5.745 GHz to 5.825 GHz.

e) Under normal operating conditions, the channel bandwidth for wireless communication of the payload network should be 20MHz.

5.1.2 The connector models and contact definitions of the load network switch are shown in Table 2. The cable/optical cable design of the wired network terminal should be compatible with them.

5.2 Link Layer

The link layer protocol of the space station payload network meets the following requirements.

a) For wired Ethernet network terminals, the link layer protocol should conform to the MAC frame format defined in IEEE std 802.3, and should not use... LLC sublayer;

b) For wireless LAN network terminals, the link layer protocol should conform to the MAC frame format defined in IEEE std 802.11 and should not use... Use LLC sublayer;

c) For wireless network terminals requiring fast roaming, the link layer protocol should comply with the IEEE std 802.11k/v/r specifications;

d) The MAC address of a network terminal should meet the requirement of global uniqueness.

5.3 Network Layer

The network layer protocol of the space station payload network must meet the following requirements.

a) The IP protocol should comply with RFC 791;

b) The ARP protocol shall comply with RFC 826;

c) The ICMP protocol shall comply with RFC 792;

d) The space station should uniformly assign IP addresses, with the gateway address being the gateway address of the module where the network terminal is located, and the subnet mask being 20 bits;

e) IP addresses should be statically assigned; DHCP should not be used.

f) In principle, multicast protocols should not be used on payload network terminals.

5.4 Transport Layer

The transport layer protocol of the space station payload network meets the following requirements.

a) The UDP protocol should comply with RFC 768;

b) The TCP protocol should comply with RFC 793;

c) Network terminals should indicate the transport protocol used by the transport layer in the protocol number field of the IP data packet.

5.5 Application Layer

In principle, there are no restrictions on the application layer protocols used for communication between network terminals or between network terminals and ground terminals. Application layer protocol symbols It meets the following requirements.

a) Network terminals that require management using a payload network manager should use the SNMP protocol and comply with RFC1905. v2c version.

b) Network terminals that require time synchronization using the payload network manager should use the SNTP protocol and comply with RFC1769 v3.

For this version, the transport layer should use the UDP protocol, and the network layer should use the IP protocol.

c) Network terminals that require data storage using a payload network manager should use the FTP or TFTP protocol, and.

1) The FTP protocol should comply with RFC 959;

2) The TFTP protocol should comply with RFC1350.

6 Other communication requirements

The following requirements must be met when the space station payload network communicates.

a) The interval between sending ARP request packets should be no less than 1 second, and the ARP aging time setting on network terminals should be less than 270 seconds, preferably [missing information]. 180s;

b) If no response is received after sending 5 consecutive ARP messages, the sending of ARP messages should be stopped, and resending may be done after 180 seconds. ARP request message;

c) It is advisable to design self-protection measures to avoid the impact on oneself when other network terminals malfunction;

d) For network terminals designed for cold backup, the primary and backup products should use the same MAC address, IP address, subnet mask, and gateway. set up;

e) For network terminals designed with hot backup, the primary and backup products should preferably use adjacent IP addresses, the same subnet mask, and gateway settings;

f) When communicating with terrestrial network terminals, the UDP protocol should be used and flow control measures should be implemented to ensure that the communication rate does not exceed the limit. Allocated bandwidth;

g) When communicating with ground network terminals, fixed-length frames should be used to transmit network data. The length of the network data frame should be consistent with the length of the space station's ground-to-space link.

The transmission efficiency is highest when the effective data field length of the transmitted frame matches.

7 Test Requirements

7.1 Before uplinking or upgrading in-orbit, network terminals should complete network communication self-testing, information security access confirmation, and space station entry confirmation.

Only after all information interface tests are passed can the system be uploaded or upgraded in orbit and used within the space station.

7.2 Before the network terminal leaves the factory or is upgraded in orbit, a network communication self-test should be completed on the ground according to the following regulations.

a) Interface performance testing, including.

1) Wired network electrical interface negotiation rate;

2) Average optical power, saturation optical power, and receiver sensitivity of the wired network fiber optic interface;

3) Communication frequency, negotiation rate, etc. of wireless networks.

b) Network protocol testing, including.

1) ARP request message format check, ARP reply message format check, request message sending frequency test, ARP table maintenance. Time-of-use testing;

2) ICMP protocol testing;

3) UDP/TCP protocol format check.

c) Business testing, including.

1) Normal communication mode test;

2) Boundary value traversal test with configurable parameters;

3) Hardware and software failure mode testing.

d) Network security testing. Conduct relevant tests using virus scanning and detection tools.

7.3 The information security access confirmation process is divided into three stages. information security design and testing review, information security evaluation, and electrical space station testing.

Specifically, it should be carried out in accordance with the relevant requirements for the information security access confirmation work of the space station.

7.4 The information interface test for space station entry confirmation shall comply with the provisions of GB/T 47455.

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 15 pages — is available in the English PDF.

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