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When the USSR started working on Mir, they were also working on the Buran shuttle program. APAS-89 was envisioned to be the docking system for Buran with the Mir space station. The APAS-75 design was heavily modified. The outer diameter was reduced from 2030 mm to 1550 mm and the alignment petals were pointed inward instead of outward.
a. ^ Although STS-96 was the first Space Shuttle mission to perform a docking maneuver with the ISS, it was not the first to visit the station. During the previous mission, STS-88, the Space Shuttle Endeavour used the Canadarm to first attach the newly delivered Unity module to its airlock, then grasp the Zarya module to join it with Unity ...
The simulation is centered on a typical Space Shuttle mission to service a space station. Mission phases include Earth Lift-Off, Orbital Rendezvous, Approach and Alignment and Docking. [2] It was released for the Apple II in 1982, [2] receiving positive feedback from reviewers. [3]
The Hubble Space Telescope received the Soft-Capture Mechanism (SCM) on STS-125. [7] The SCM is meant for unpressurized docking, but uses the LIDS interface to reserve the possibility of an Orion docked mission. [7] The docking ring is mounted on Hubble's aft bulkhead. [7] It may be used for safely de-orbiting Hubble at the end of its service ...
The docking mechanism of the Apollo was a "probe and drogue" system designed to allow the Apollo Command/Service Module (CSM) to dock with the Apollo Lunar Module.The same system was later used for the Skylab 2, Skylab 3 and Skylab 4 CSMs to dock with the Skylab space station, and the Apollo–Soyuz Test Project CSM to dock with a Docking Module adapter which allowed docking with the Soyuz 19 ...
The R-bar pitch maneuver (RPM), popularly called the rendezvous pitch maneuver or backflip, [1] was a maneuver performed by the Space Shuttle as it rendezvoused with the International Space Station (ISS) prior to docking. The Shuttle performed a backflip that exposed its heat-shield to the crew of the ISS that made photographs of it. Based on ...
The Rendezvous Docking Simulator, also known as the Real-Time Dynamic Simulator, is a simulator at the Langley Research Center. It was constructed for the Gemini program in Building 1244 and it became operational in June 1963 at a cost of $320,000 [ 4 ] and later reconfigured for the Apollo program. [ 4 ]
The US space program's concept of berthing was developed to mitigate issues of orbital mechanics that were encountered during the evolution of docking. Although not the first mechanism developed specifically for berthing, the CBM was the first such device designed in the US specifically to assemble structural joints that would hold sea-level ...