XSS-10 (eXperimental Small Satellite 10) was a small, low-cost micro-spacecraft developed by the U.S. Air Force Research Laboratory's Space Vehicles Directorate to test technology for …

2024年4月20日 · XSS-10 (Experimental Small Satellite 10), a 28 kilogram microsatellite, was launched as a secondary payload aboard a Delta-7925 launch vehicle carrying a Global …

Boeing XSS-10 Launched on 30 January 2003 with a Delta 7925-9.5 launcher from Cape Canaveral, the experimental XSS-10A satellite was developed by the U.S. Air Force to …

The XSS-10 is a micro-satellite system used for testing telemetry tracking and command (TT&C) systems using the Air Force Satellite Control Network (AFSCN). The state-of-the-art …

2003年1月29日 · XSS-10. The first experimental mission, named XSS-10, is a joint effort among the following partners: AFRL, NASA, NRL and the Lawrence Livermore Laboratory. …

The mission objectives of XSS-10 were to demonstrate autonomous navigation, proximity operations, and inspection of a Resident Space Object (RSO). XSS-10 was a 28-kilogram …

The XSS-10 micro-satellite demonstration was the first in a series of micro-satellites to be used for important future Air Force space missions. The XSS-10 is a building block for future space …

实验小卫星10号（Experimental Small Satellite 10）是美国空军研究实验室（AFRL）/美国国防部（DoD）的一项技术演示微型卫星（重28 kg），于2003年1月29日世界时18:06由德尔塔2运 …

The XSS-10 system consisted of six major elements — the Micro-Sat, an expendable launch vehicle (ELV), the Sconce Payload Platform (SPP), the Sconce Electronics Platform (SEP), …

美国试验小卫星xss_10系统-集成活动包括多项功能测试、 射频兼容性测试、燃料添加和耐压测试、测量带燃料的小卫星的重心 和惯性矩、与德尔它 2 组装。