The invention discloses a configurable carrier rocket multi-satellite launching control system, and relates to the technical field of spaceflight, and the system comprises a satellite-rocket separation control combination, at least one flight control combination, a resistor box used for protecting a satellite-rocket separation time sequence path, and a plurality of satellite separation mechanisms used for satellite installation and separation. Wherein the satellite-rocket separation control combination, each flight control combination and each satellite separation mechanism are all connected with the resistance box; and the satellite-rocket separation control combination communicates with the flight control combination. Under the condition that an original carrier rocket satellite separation control scheme is not changed, more time sequence control is provided by newly adding a satellite-rocket separation control combination, the carrier rocket satellite separation time sequence is greatly increased, and the number of multiple satellites in one rocket is greatly increased.
本申请公开了一种可配置的运载火箭多星发射控制系统,涉及航天技术领域,包括:星箭分离控制组合、至少一个飞行控制组合、用于保护星箭分离时序通路的电阻盒和多个用于卫星安装与分离的卫星分离机构;其中,星箭分离控制组合、每个飞行控制组合和每个卫星分离机构均与电阻盒连接;星箭分离控制组合与飞行控制组合通信。本申请在不更改原有运载火箭卫星分离控制方案的情况下,通过新增一个星箭分离控制组合,以提供更多的时序控制,实现运载火箭卫星分离时序的大量增加,大幅提高了一箭多星的数量。
Configurable carrier rocket multi-satellite launch control system
一种可配置的运载火箭多星发射控制系统
2025-04-25
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
CARRIER ROCKET SYSTEM WITH CARRIER ROCKET AND LAUNCH ASSISTANCE UNIT
European Patent Office | 2022
|One Rocket Multiple Satellite Launch Technology
NTIS | 1982
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