MarketAndrogynous Peripheral Attach System
Company Profile

Androgynous Peripheral Attach System

The terms Androgynous Peripheral Attach System (APAS), Androgynous Peripheral Assembly System (APAS) and Androgynous Peripheral Docking System (APDS) are used interchangeably to describe a Russian family of spacecraft docking mechanisms, and are also sometimes used as generic names for any docking system in that family. A system similar to APAS-89/95 is used by the Chinese Shenzhou spacecraft.

Overview
The name of the system is Russian in origin, and is an acronym, , in the Cyrillic alphabet, from the Russian (Androginno-periferiynyy agregat stykovki). The English acronym was designed to be just the same letters but in the Latin alphabet, for which the first two words are direct counterparts of those in the original. The third word in Russian comes from the German , meaning "complicated mechanism", and the last means "docking". The last two words in the English name were picked to begin with the same equivalent letters as in the Russian name. The idea behind the design is that unlike with the probe-and-drogue docking system, any APAS docking ring can mate with any other APAS docking ring; both sides are androgynous. In each docking there is an active and a passive side, but both sides can fulfill either role. There are three basic variations of the APAS. ==APAS-75==
APAS-75
Co-developed by American and Soviet engineers through a series of in-person meetings, letters and teleconferences, APAS-75 was initially planned to be used on an American mission to a Salyut space station which instead became Apollo–Soyuz. The device is called the Androgynous Peripheral Docking System (APDS) in the NASA press packet for ASTP. The Americans selected North American Rockwell to construct seven docking mechanisms (two flight, four test, and one spare). The Soviet Union built five Soyuz spacecraft that used APAS-75. The first three flew as test systems (Cosmos 638, Cosmos 672 and Soyuz 16). The fourth one was used for the Apollo-Soyuz Test Project, Soyuz 19 the only Soyuz to actually use the docking system, while the last APAS-75 fitted to Soyuz 22 was replaced by a camera prior to flight. On the American side the Apollo–Soyuz Docking Module carried one APAS-75 docking collar and one Apollo docking collar. Development In April 1970 NASA Administrator Thomas O. Paine suggested, in an informal meeting with Russian academician Anatoli Blagonravov in New York, that the two nations cooperate on astronaut safety, including compatible docking equipment on space stations and spacecraft to permit rescue operations in space emergencies. Engineer Caldwell Johnson proposed a ring and cone system during a meeting in Moscow during October 1970. Boris N. Petrov rejected the simple adaptation of Apollo and Soyuz as a "space stunt" and had proposed developing a universal docking mechanism, Johnson suggested that the Manned Spacecraft Center (MSC) draw up a "design specifically adequate to requirements of a particular CSM/Salyut mission, the design being representative only of the fundamental form and function of docking gear satisfying the requirements for compatible docking system for future spacecraft." Larry Ratcliff drew the capture ring and guides on drafting paper, and Robert McElya supplied the details of the structural interface ring, while Bobrov prepared a similar drawing for the structural latches. Final official approval of a joint docking mission came in Moscow on 24 May 1972. U.S. President Nixon and U.S.S.R. Premier Aleksey N. Kosygin signed the Agreement Concerning Cooperation in the Exploration and Use of Outer Space for Peaceful Purposes, including development of compatible spacecraft docking systems to improve safety of manned space flight and to make joint scientific experiments possible. Some refinements were made in the guides and other parts of the mechanism; as with the other groups, a schedule for the upcoming months was written, indicating documents to be prepared and tests to be conducted. Some of the Americans observed that while the U.S.S.R. mechanism was more complex mechanically than the American one, it was suitable for the mission and "sophisticated" in its execution. The Americans arrived in Moscow on December 6 and worked through December 15. ==APAS-89==
APAS-89
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. This limited the internal passage diameter of the docking port to about 800 mm. The Buran shuttle was finally canceled in 1994 and never flew to the Mir space station, but Mir's Kristall module was outfitted with two APAS-89 docking mechanisms. The Mir Docking Module, basically a spacer module between Kristall and the Shuttle, also used APAS-89 on both sides. ==APAS-95==
APAS-95
APAS was selected for the Shuttle-Mir program and manufactured by Russian company RKK Energiya under an $18 million contract signed in June 1993. Rockwell International, prime contractor for the Shuttle, accepted delivery of hardware from Energiya in September 1994 It had a mass of 286 kg. APAS-95 was selected to join the American and Russian modules on the International Space Station (ISS) and to allow the Space Shuttle to dock. The Shuttle's Orbiter Docking System remained unchanged from when it was used for the Shuttle–Mir Program in 1995. The active capture ring that extends outward from the spacecraft captured the passive mating ring on the space station's APAS-95 connection on the Pressurized Mating Adapter. The capture ring aligned them, pulled them together and deployed 12 structural hooks, latching the two systems with an airtight seal. The Pressurized Mating Adapters are permanently passive. ==ASA-G/ASP-G==
ASA-G/ASP-G
The ASA-G is used only by the Nauka Science (or Experiment) Airlock to berth to the Nauka forward port on 4 May 2023, 01:00 UTC during VKD-57 spacewalk. The non-androgynous berthing mechanism is a unique hybrid derivative of the Russian APAS-89/APAS-95 system, as it has 4 petals instead of 3 along with 12 structural hooks and is a combination of an active "probe and drogue" soft-dock mechanism on port and passive target on airlock. ==Images==
Images
Image:STS-76 docking with MIR.jpg|APAS in a Shuttle–Mir docking Image:Orbiter Docking System (STS-98).jpg|Orbiter Docking System (bottom, white), APAS-95 (middle, white/gray) and PMA-3 (top, black/grey) ==See also==
tickerdossier.comtickerdossier.substack.com