ISRO के वैज्ञानिक SPADEX के गुप्त मॉड्यूल में 4 दिन से कर रहे थे महाएक्सपेरिमेंट, मचा तगड़ा भौकाल скачать в хорошем качестве

ISRO के वैज्ञानिक SPADEX के गुप्त मॉड्यूल में 4 दिन से कर रहे थे महाएक्सपेरिमेंट, मचा तगड़ा भौकाल

ISRO के वैज्ञानिक SPADEX के गुप्त मॉड्यूल में 4 दिन से कर रहे थे महाएक्सपेरिमेंट, अब मचा हड़कंप Mission SPADEX Launch LIVE | ISRO LIVE | "ISRO का SpaDeX (Space Docking Experiment) मिशन भारत को अंतरिक्ष में नई ऊंचाईयों पर ले जा रहा है! जानिए कैसे यह मिशन भारत को अंतरिक्ष तकनीकों में सुपरपावर बना रहा है। दो स्पेसक्राफ्ट्स की ऐतिहासिक डोकिंग और इस मिशन से जुड़ी हर रोमांचक जानकारी। देखिए इस अद्भुत मिशन की कहानी।" #ISRO #SpaDeXMission #SpaceDocking #IndianSpaceProgram #ISROAchievements #अंतरिक्ष_में_भारत #IndianInnovation #SelfReliantIndia #SpaceExploration #ISROTechnology #ISROMission #IndiaInSpace #SpaDeXIndia SpaDeX mission is a cost-effective technology demonstrator mission for the demonstration of in-space docking using two small spacecraft launched by PSLV. This technology is essential for India’s space ambitions such as Indian on Moon, sample return from the Moon, the building and operation of Bharatiya Antariksh Station (BAS), etc. In-space docking technology is essential when multiple rocket launches are required to achieve common mission objectives. Through this mission, India is marching towards becoming the fourth country in the world to have space docking technology. The primary objective of the SpaDeX mission is to develop and demonstrate the technology needed for rendezvous, docking, and undocking of two small spacecraft (SDX01, which is the Chaser, and SDX02, the Target, nominally) in a low-Earth circular orbit. Secondary objectives include: Demonstration of the transfer of electric power between the docked spacecraft, which is essential for future applications such as in-space robotics, Composite spacecraft control, and Payload operations after undocking. More Details The SpaDeX mission consists of two small spacecraft (about 220 kg each) to be launched by PSLV-C60, independently and simultaneously, into a 470 km circular orbit at 55° inclination, with a local time cycle of about 66 days. The demonstrated precision of the PSLV vehicle will be utilized to give a small relative velocity between the Target and Chaser spacecraft at the time of separation from the launch vehicle. This incremental velocity will allow the Target spacecraft to build a 10-20 km inter-satellite separation with respect to the Chaser within a day. At this point, the relative velocity between the Target will be compensated using the propulsion system of the Target spacecraft. At the end of this drift arrest maneuver, the Target and Chaser will be in the same orbit with identical velocity but separated by about 20 km, known as Far Rendezvous. With a similar strategy of introducing and then compensating for a small relative velocity between the two spacecraft, the Chaser will approach the Target with progressively reduced inter-satellite distances of 5 km, 1.5 km, 500 m, 225 m, 15 m, and 3 m, ultimately leading to the docking of the two spacecraft. After successful docking and rigidization, electrical power transfer between the two satellites will be demonstrated before undocking and separation of the two satellites to start the operation of their respective payloads for the expected mission life of up to two years.