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Pressurized Mating Adapter
Pressurized Mating Adapter
Pressurized Mating Adapter
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Pressurized Mating Adapter
PMA-2 attached to the forward port of Destiny, where it was located between 2001 and 2007
Module statistics
Part ofInternational Space Station
Launch date
  • PMA-1 & 2: December 4, 1998
  • PMA-3: October 11, 2000
Launch vehicleSpace Shuttle
Docked
  • PMA-1 & 2: December 7, 1998
  • PMA-3: October 13, 2000

A Pressurized Mating Adapter (PMA) is a component used on the International Space Station (ISS) to convert the Common Berthing Mechanism (CBM) interface used to connect ISS modules to an APAS-95 spacecraft docking port. Three PMAs are attached to the US Orbital Segment of ISS. PMA-1 and PMA-2 were launched along with the Unity module in 1998 aboard STS-88; PMA-3 was launched in 2000 aboard STS-92. PMA-1 permanently connects the Unity and Zarya modules. International Docking Adapters were permanently installed on PMA-2 and PMA-3 in 2017 to convert them from the APAS-95 standard to the newer International Docking System Standard (IDSS).

Design and history

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Its origins lie in designs for the Pressurized Docking Mast,[1] consisting of an off-axis frustoconical docking tunnel contained within a framework and a retractable coupling mechanism, later part of the Pressurized Berthing Adapter assembly that appeared in designs for Space Station Freedom 1987, and the reduced design referred to as 'Fred'[2] 1991.

After 1992–1993 and the Russian integration into the International Space Station Alpha project,[3][4] this NASA docking design abruptly disappeared from all concepts.[5] This was due to the availability of Russian docking hardware and experience, brought together during the Shuttle–Mir program.[6] Russian APAS docking technology originally planned for the then defunct Soviet space shuttle program was integrated into the US Space Shuttle ODS (Orbital/Orbiter Docking System).[7] This could hard dock with the space station through a structural interface, which became the PMA.[8] With both the Russian docking ring and the CBM integrated into the PMA, this became the link between the USOS and the ROS from 1993.

Fabrication completed in 1995 with tests and mating tests with Node STA throughout 1996–97.[9]

Space Station Freedom configuration 1991

Uses

[edit]
Expedition 58 crew member Anne McClain inside PMA-1, with the interior of Zarya in the background. PMA-1 has served as the bridge between Zarya and Unity since the modules were berthed in 1998.

The three PMAs are identical,[10] but they have slightly different uses. All three perform the same basic function of connecting a CBM port of an ISS module to an APAS-95 docking port of another module or visiting spacecraft.[11] For this purpose, the PMAs carry a passive CBM port and a passive APAS port. The PMAs are pressurized and heated from the inside, and they allow for power and data communications transfer through docking rings and external connections.[12]

PMA-1

[edit]

This was one of the first components of the ISS (International Space Station). PMA-1 joins the Russian side of the station with the US side. On STS-88, the crew used the shuttle's robotic arm to attach the Zarya control module to PMA-1, which was already connected to the aft berthing port of Unity. These first two station components are permanently connected by PMA-1.

PMA-2

[edit]
Locations of PMA-2 and PMA-3 on the forward and zenith ports of Harmony, with International Docking Adapters attached to convert the APAS-95 ports to IDSS

PMA-2 is mounted on the forward port of the Harmony connecting node, and was used when Space Shuttle orbiters docked at the ISS. It was outfitted with Station-to-Shuttle Power Transfer System (SSPTS) hardware to allow the shuttles to stay docked longer to the space station.[13]

PMA-2 was moved several times as part of the space station assembly process. It was originally connected to the forward hatch of Unity, but when STS-98 delivered the Destiny module in February 2001, PMA-2 was moved to the berthing ring of the Z1 truss so that Destiny could be berthed to the forward hatch of Unity. PMA-2 was then moved to the forward hatch of Destiny.[14] (The removal of PMA-2 from Unity was the first time the CBM had been used to disconnect two ISS components.)[15] After STS-120 had delivered Harmony to the space station in October 2007, Canadarm2 repositioned PMA-2 at the forward port of Harmony on November 12, 2007. Two days later, the combined package of Harmony and PMA-2 was moved to its final location, the forward hatch of Destiny. On July 18, 2016, International Docking Adapter-2 was launched on SpaceX CRS-9.[16] It was attached and permanently connected to the APAS-95 port of PMA-2 during a spacewalk on August 19, 2016.[17] As of 2020, PMA-2 is expected to stay berthed at the forward port of Harmony with the IDA connected for the remaining duration of the ISS.

When a shuttle docked with the station, its "final approach [was] at a relative velocity of one-tenth of a foot per second. [As it made] contact with Pressurized Mating Adapter 2 [latches] automatically attached the two spacecraft together. Once relative motion between the spacecraft stopped, [a Shuttle astronaut retracted] the docking ring on [the Shuttle's] mechanism, closing latches to firmly secure the shuttle to the station."[18]

PMA-3

[edit]
PMA-3 with IDA-3, attached to the zenith berth of the Harmony module, November 2024

PMA-3 was brought to the ISS by STS-92 in October 2000, mounted on a Spacelab pallet.[19] It was initially attached to the nadir (Earth-facing) berth of Unity. About six weeks later, when STS-97 delivered the P6 solar array truss structure, Endeavour docked at PMA-3.[20] When STS-98 moved PMA-2 from Unity to Destiny via the Z1 truss in February 2001, Atlantis was docked at PMA-3.[14] For the remainder of the shuttle's operation, PMA-3 was not used for shuttle dockings. PMA-3 was moved in March 2001 to Unity's port berth by the crew of STS-102 to make room for the docking of the Multi-Purpose Logistics Module (MPLM).[21]

On August 30, 2007, PMA-3 was returned to the nadir port of Unity to make room for the temporary docking of the Harmony (Node 2) module that was delivered by STS-120.[22] Harmony was transferred to the forward port of Destiny, while PMA-3 was moved back to the port berthing mechanism of Unity on August 7, 2009, to accommodate reconfiguration of the Unity port bulkhead by crew members in a pressurized environment.[23] On January 25, 2010, PMA-3 was moved from the port berthing mechanism of Unity to the zenith (space-facing) port of Harmony to make room for the Tranquility (Node 3) module which was added to the station during STS-130. After activation of Tranquility, PMA-3 was moved again on February 16, 2010, to the port location on Tranquility where the Cupola observatory module had been docked for launch.[24]

PMA-3 was robotically removed from Tranquility on March 26, 2017, and again attached to the zenith berth of Harmony after being prepared during a successful spacewalk on March 24, 2017. A second spacewalk was conducted on March 30, 2017, to finalize the PMA-3 cable connections on Harmony. PMA-3 received International Docking Adapter-3 in August 2019.[25]

References

[edit]
[edit]
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Pressurized Mating Adapter

View on Grokipedia
from Grokipedia
A Pressurized Mating Adapter (PMA) is a conical docking interface component integral to the International Space Station (ISS), designed to convert the approximately 1.3-meter U.S. Common Berthing Mechanism (CBM) for module berthing into the approximately 1.55-meter outer diameter Russian Androgynous Peripheral Attachment System (APAS-95) for spacecraft docking, with an inner passage of about 0.8 meters, enabling seamless connections between American and Russian-built elements while supporting environmental control and life support functions such as air, oxygen, nitrogen, and water transfer. Developed by Boeing for NASA, the three PMAs—PMA-1, PMA-2, and PMA-3—were launched aboard Space Shuttle missions: PMA-1 and PMA-2 on STS-88 in December 1998 to initially link the U.S. Node 1 (Unity) to the Russian Zarya module, and PMA-3 on STS-92 in October 2000 to serve as an additional docking port. Each PMA features a mass ranging from 1,200 to 1,600 kg, lacks independent propulsion, and relies on ISS power, with PMA-1 lacking a hatch while PMA-2 and PMA-3 include APAS hatches for direct spacecraft access. Their slanted, cone-shaped design provides clearance for large payloads during extravehicular activities and accommodates the Space Shuttle's docking geometry. Over time, PMA-2 and PMA-3 have been relocated multiple times by robotic arms and spacewalks to adapt to evolving ISS configurations, such as moving PMA-2 from Node 1 to the Destiny laboratory's forward hatch in 2001 and PMA-3 to Node 3's forward port in 2010. In the post-Shuttle era, they support commercial crew vehicles through the addition of International Docking Adapters (IDAs); IDA-2 was installed on PMA-2 at the Harmony module's forward port in 2016, and IDA-3 on PMA-3 at the zenith port in 2019, adhering to the International Docking System Standard for compatibility with spacecraft like SpaceX Crew Dragon and Boeing Starliner. The PMAs' environmental systems, including temperature-controlled ventilation (65–85°F at 120–148 cfm flow rates) and high-pressure gas lines with quick-disconnect fittings, ensure crew safety by maintaining atmospheric integrity and facilitating resource distribution across the station. As of 2025, all three remain operational, underscoring their enduring role in ISS assembly, maintenance, and future deep-space transition efforts.

Overview

Purpose and Role in ISS

The Pressurized Mating Adapter (PMA) serves as a short, pressurized conical tunnel designed to convert the U.S. Common Berthing Mechanism (CBM) interface—used for berthing larger modules to the International Space Station (ISS)—to the Russian Androgynous Peripheral Attach System (APAS-95) docking port, which accommodates smaller docking spacecraft. This adaptation allows compatibility between the differing docking standards of the U.S. Orbital Segment and the Russian Orbital Segment, enabling seamless connections without altering the core infrastructure of either side. In its role within the ISS, the PMA maintains a sealed, pressurized environment to ensure crew safety and operational continuity during module integrations or spacecraft dockings, while also incorporating subsystems for temperature and humidity control to regulate thermal conditions within the adapter. It further contributes to structural integrity by providing a robust mechanical interface that distributes loads across connected elements, preventing stress concentrations during orbital maneuvers or dynamic events. These functions collectively support the station's habitability and reliability as a long-duration outpost. The PMA's primary importance lies in facilitating the modular assembly of the ISS, which integrated diverse international contributions by bridging incompatible docking architectures and avoiding costly redesigns of existing hardware. By enabling direct connections between U.S. nodes and Russian modules, it streamlined construction phases and enhanced interoperability. Moreover, PMAs support essential utility transfers, including power, data, and fluids—such as scavenging excess water and air from docked vehicles like the Space Shuttle—between the station and visiting elements, thereby optimizing resource management.

Key Components and Compatibility

The Pressurized Mating Adapter (PMA) consists of a conical pressure vessel approximately 1.8 meters in length, tapering from 1.3 meters in diameter at the Common Berthing Mechanism (CBM) end to 0.8 meters at the Androgynous Peripheral Attach System (APAS-95) end, which maintains structural integrity and pressurization within the International Space Station (ISS) environment. This vessel is integrated with conical end sections that incorporate the Common Berthing Mechanism (CBM) port on one end for attachment to ISS modules and the Androgynous Peripheral Attach System (APAS-95) port on the other for docking with visiting vehicles. An internal tunnel spans the adapter, providing a passageway for crew transfer between connected elements while supporting environmental control and life support functions such as ventilation. PMA-2 and PMA-3 are identical in design and construction, having been manufactured by McDonnell Douglas Aerospace (now Boeing) to ensure uniformity in interfacing capabilities, while PMA-1 shares a similar overall design but lacks an APAS hatch. The adapters operate as passive components, devoid of independent active docking or attachment mechanisms, which places the responsibility for alignment, capture, and soft docking on the approaching spacecraft or module. This design simplifies the PMA's role to that of a structural and pressurized bridge, minimizing complexity and mass while facilitating reliable connections. In terms of compatibility, the APAS-95 port on the PMA enables docking with Space Shuttle Orbiters equipped with compatible systems, allowing for pressurized crew and cargo transfer. The CBM port interfaces seamlessly with U.S. and international ISS modules, such as nodes and laboratories, supporting berthing operations. To accommodate modern commercial crew vehicles, PMAs have been adapted for the International Docking System Standard (IDSS) through the attachment of International Docking Adapters (IDAs), which provide standardized ports for spacecraft like Boeing's Starliner and SpaceX's Crew Dragon, including provisions for power, data, and communication transfer.

Design and Specifications

Structural and Material Features

The Pressurized Mating Adapter (PMA) is engineered as a truncated conical aluminum pressure vessel to ensure structural integrity while providing a sealed, pressurized pathway between incompatible docking interfaces on the International Space Station (ISS). This design accommodates the axial offset of 28 inches (71 cm) between its end rings, allowing alignment with both the U.S. Common Berthing Mechanism (CBM) at the wider end and the Russian Androgynous Peripheral Attach System (APAS) at the narrower end. Key dimensions include a length of 1.86 m (6.1 ft), a diameter of 1.9 m (6.25 ft) at the wide end, and 1.37 m (4.5 ft) at the narrow end, with masses varying by unit: PMA-1 at 1,589 kg (3,504 lb), PMA-2 at 1,376 kg (3,033 lb), and PMA-3 at 1,183 kg (2,607 lb). The aluminum construction, combined with multi-layer insulation (MLI) thermal blankets on the exterior, offers protection against micrometeoroids and orbital debris (MMOD) impacts while regulating surface temperatures across the ISS external operating range of approximately -150°C to +120°C. These blankets also mitigate thermal extremes from solar exposure and deep space cold, contributing to the overall durability in low Earth orbit. The PMA's structure is qualified to withstand launch vibrations through protoflight testing protocols, orbital dynamic stresses, and internal pressure differentials of up to 1 atm, ensuring reliability over the ISS's baseline 15-year design life, which has since been extended. Internal heating elements maintain habitable conditions to prevent condensation on surfaces during operations, while external features include handrails for extravehicular activity (EVA) mobility and berthing guides to facilitate robotic arm capture and alignment during installation or relocation. The design supports multiple docking and undocking cycles, as demonstrated by PMA-2's repeated use for Space Shuttle missions.

Docking and Interface Mechanisms

The Pressurized Mating Adapter (PMA) serves as a critical interface on the International Space Station (ISS), enabling the connection of modules via the Common Berthing Mechanism (CBM) on one side and active docking with visiting vehicles, such as the Space Shuttle, via the Androgynous Peripheral Attachment System (APAS-95) on the other. The docking process with APAS-95 begins with coarse alignment as the incoming vehicle approaches the PMA, utilizing guide petals and a probe-drogue configuration for initial contact. Soft capture occurs when the vehicle's probe engages the PMA's drogue receptacle, followed by the extension of a guide ring to attenuate any residual misalignment and secure initial attachment. This phase transitions to hard mate, where 12 powered hooks and latches engage to provide structural rigidity, aligning the vehicles to within millimeters for a stable connection. Once hard mate is achieved, the PMA supports pressurization of the interconnecting volume through dedicated umbilical lines and quick-disconnect fittings, allowing the transfer of high-pressure oxygen and nitrogen gases while equalizing cabin pressures between the ISS and the docked vehicle. Hatch opening follows leak checks, enabling crew transfer and resource sharing. The CBM side, in contrast, supports berthing operations for passive module attachment using 16 powered bolts for structural fixation after robotic positioning, but the PMA's dual-interface design uniquely converts this berthing-only mechanism into an active docking port capable of independent vehicle approach and capture. Redundancy in the system includes multiple alignment guides and latch mechanisms to ensure reliable capture under varying orbital conditions. The PMA incorporates standardized electrical and data interfaces to facilitate power and command/telemetry exchange between the ISS and docked elements. Electrical connectors provide 120 V DC power distribution, capable of transferring up to 3 kW to support vehicle systems and payloads during mating. Data interfaces employ the MIL-STD-1553 multiplexed serial bus for real-time command, control, and telemetry, ensuring compatibility across U.S. and international segments, while Ethernet links handle higher-bandwidth video and payload data. These interfaces activate automatically during hard mate via retractable connectors, with umbilicals providing continuous connectivity for utilities like thermal control and propulsion propellant transfer. Seals around the APAS hatch and CBM ports maintain airtight integrity, preventing pressure loss during operations.

Development History

Origins in Early Space Station Concepts

The Pressurized Mating Adapter (PMA) originated in the design efforts for the United States' Space Station Freedom (SSF) program during the late 1980s. In 1987, NASA developed the concept of the Pressurized Docking Mast (PDM) as a core element of the SSF architecture, specifically to enable connections between the Space Shuttle Orbiter and station modules for crew transfer, resupply, and assembly operations. The PDM was engineered as a pressurized crew transfer tunnel integrated into the Orbiter Attachment System, featuring a slide track capture device to align the Orbiter with the forward berthing ports on Resource Nodes 3 and 4, thereby maintaining a continuous pressurized environment between the vehicles. Initial contracts for SSF's pressurized elements, encompassing early docking system designs like the PDM, were awarded to Rockwell International and McDonnell Douglas Corporation in 1985 under NASA's Phase B studies, positioning both companies as lead contractors for the station's manned modules and structural framework. Their contributions focused on integrating Shuttle-compatible interfaces to support modular station growth and logistics delivery. Prototypes of the evolving PMA components underwent qualification testing for pressure containment, thermal vacuum cycling, and structural integrity under launch and orbital conditions to ensure operational reliability. By 1991, escalating costs prompted a comprehensive redesign of the SSF program, emphasizing modularity and efficiency, which incorporated the Common Berthing Mechanism (CBM) to standardize attachments for growth modules and vehicles. This redesign transformed the PDM into the foundational PMA configuration, shifting to a male/female active-passive berthing system with internal alignment guides, elastomeric seals, capture latches, and powered bolts on 2.0-meter structural rings to facilitate robotic berthing without extensive extravehicular activity. The Boeing Company led the detailed CBM development under NASA oversight, building on prior neutral buoyancy simulations and component tests. The post-1992 Shuttle-Mir program further shaped the PMA by necessitating compatibility with Russian hardware, leading to the integration of the Androgynous Peripheral Attachment System (APAS) as a docking interface to accommodate Soyuz and Progress vehicles alongside Shuttle operations. This adaptation, evaluated by NASA engineering teams, enhanced cross-system interoperability and informed subsequent international station designs.

Adaptation for International Space Station

Following the 1993 reconfiguration of the International Space Station (ISS) program, which incorporated Russian contributions to create a U.S.-Russian hybrid architecture, the Pressurized Mating Adapter (PMA) underwent significant redesign between 1993 and 1995 to shift from an initial mast-based docking concept in early Space Station Freedom plans to a dedicated conical adapter for seamless integration with both U.S. Common Berthing Mechanism (CBM) ports and Russian docking systems. This adaptation ensured compatibility with the Russian Functional Cargo Block (FGB) module and orbiter docking requirements, addressing structural loads up to 1,200 pounds from the Russian system while maintaining the original 400-pound U.S. design limit through modifications to power systems and berthing interfaces. The redesign emphasized modular connectivity across ISS nodes, with PMAs positioned on axial and radial ports to facilitate pressurized module attachments without the need for intermediate masts. Fabrication of the PMAs was completed by McDonnell Douglas Aerospace (acquired by Boeing in 1997) in Huntington Beach, California, in 1995, utilizing four circumferentially welded Aluminum 2219 forgings for the primary structure, along with thermal insulation blankets and 52 electrical fittings to support environmental control and life support systems. A production readiness review conducted on March 14, 1995, confirmed the manufacturing processes, including variable polarity plasma arc (VPPA) welding refinements after initial development unit discrepancies. Three units—PMA-1, PMA-2, and PMA-3—were produced to outfit key ISS locations, providing redundant docking ports for assembly and operations. Qualification testing occurred from 1996 to 1997 at NASA's Marshall Space Flight Center, encompassing vibration, acoustic, thermal vacuum, and proof pressure evaluations to 1.5 times the maximum design pressure of 16.0 psia, verifying structural integrity under on-orbit dynamic loads and microgravity conditions. These tests, detailed in the May 1996 structural integrity report (MDC 95H0336), also included integrated mating simulations with Node structural test articles to ensure berthing reliability. The adaptation culminated in the finalization of APAS-95 integration on the PMA forward end, a modified Androgynous Peripheral Attach System derived from Apollo-Soyuz heritage, compatible with the Space Shuttle's Orbiter Docking System to enable hybrid U.S.-Russian pressurization and crew transfer. This adaptation supported the international integration of the ISS, including the berthing of PMA-1 between Node 1 and the FGB (Zarya) during STS-88, establishing protocols for U.S.-Russian module connectivity.

Operational Deployment

PMA-1 Configuration and Missions

The Pressurized Mating Adapter-1 (PMA-1) was launched on December 4, 1998, aboard Space Shuttle Endeavour during mission STS-88 as part of the Unity (Node 1) module payload. PMA-1 was pre-integrated to Unity's aft Common Berthing Mechanism (CBM) port prior to launch, serving as the interface for connecting the U.S.-built Unity to the Russian Zarya module already in orbit. During the mission, the shuttle's remote manipulator system (SRMS) grappled Zarya on December 6, 1998, and maneuvered it for structural mating to PMA-1 at 9:48 p.m. EST, marking the initial assembly of the International Space Station (ISS). Following structural engagement, PMA-1 achieved full pressurized mating between the U.S. and Russian segments on December 7, 1998, when the internal pressure was equalized to 13.03 psia and subsequently repressurized to 15.0 psia, enabling a continuous pressurized pathway through the adapter. This configuration permanently affixed PMA-1 to Unity's aft CBM port, with its Androgynous Peripheral Docking System (APDS) end docked to Zarya's forward port, forming the foundational link of the ISS core structure. The adapter has remained in this fixed position since installation, oriented along the station's longitudinal axis without any relocations. PMA-1 played a critical role in early ISS assembly missions by providing the essential pressurized tunnel for crew transfer and operations between Zarya and Unity, supporting subsequent dockings such as those of the Zvezda module in 2000 and early logistics flights. Its static placement ensured reliable connectivity for power, data, and environmental control systems across the nascent station, facilitating the integration of additional elements without interruption. Unlike other PMAs, PMA-1's permanent role precluded any need for repositioning, underscoring its foundational status in the ISS architecture.

PMA-2 Relocations and Upgrades

PMA-2 launched on December 4, 1998, aboard the Space Shuttle Endeavour during mission STS-88, serving as the first U.S. assembly flight for the International Space Station (ISS). It was initially attached to the forward port of the Unity node (Node 1) to provide a docking interface compatible with the Space Shuttle's orbiter docking system. This placement allowed for subsequent shuttle visits while Unity was connected to the Zarya module via PMA-1 on its aft port. In February 2001, during the STS-98 mission, PMA-2 was relocated from the forward port of Unity—via a temporary position on the Z1 truss—to the forward port of the newly delivered Destiny laboratory module. Astronauts Thomas Jones and Mark Lee, supported by pilot Marsha Ivins using the shuttle's Remote Manipulator System, guided the adapter into place during Extravehicular Activity (EVA) 2, which lasted 6 hours and 50 minutes. This move optimized shuttle docking access to the U.S. segment and supported ongoing station assembly. A further relocation occurred in November 2007 as part of the STS-120 mission, which delivered the Harmony node (Node 3). Expedition 16 crew members Daniel Tani and Peggy Whitson, using the Canadarm2 robotic arm, detached PMA-2 from Destiny's forward port and reattached it to Harmony's forward port after Harmony was temporarily berthed to Unity. This repositioning, completed on November 12, cleared the Destiny forward port for additional modules and positioned PMA-2 to serve as the primary shuttle docking port for the expanded U.S. segment, facilitating Harmony's role in connecting European and Japanese elements. To enable compatibility with next-generation commercial crew vehicles, PMA-2 received significant upgrades starting in 2016. During Expedition 48, on August 19, the first of three spacewalks installed the International Docking Adapter-2 (IDA-2), delivered by SpaceX's CRS-9 mission, onto PMA-2's forward end at Harmony's port. Astronauts Jeffrey Williams and Kathleen Rubins connected power, data, and video cables during EVA-36, marking the first attachment to PMA-2 since the shuttle era. This upgrade converted the adapter from the legacy APAS-95 standard to the International Docking System Standard (IDSS), allowing automated dockings by SpaceX's Crew Dragon and Boeing's Starliner spacecraft. By March 2017, final internal outfitting and testing confirmed full IDSS operational status, with PMA-2 supporting its first Crew Dragon docking in 2019. Throughout its history, PMA-2 has been involved in multiple robotic operations using Canadarm2, underscoring its adaptability in supporting Node 3 expansion and ISS evolution.

PMA-3 Installations and Maintenance

PMA-3 was launched on October 11, 2000, aboard Space Shuttle Discovery during the STS-92 mission and initially attached to the starboard Common Berthing Mechanism (CBM) port of the Unity node module. This installation provided an additional docking port for subsequent shuttle missions, enabling the continued assembly of the International Space Station (ISS). In March 2001, during STS-102, PMA-3 was relocated from Unity's starboard CBM to its port CBM. In August 2007, during Expedition 15, PMA-3 was relocated from Unity's port CBM to Unity's nadir CBM using the Canadarm2 robotic arm. This move cleared the port for Harmony's temporary berthing during STS-120 and supported the addition of international partner laboratories like Columbus. In January 2010, during Expedition 22, PMA-3 was relocated from Unity's nadir to Harmony's zenith port. It was then moved to Node 3's port in February 2010. PMA-3 underwent further relocation in March-April 2017 during Expeditions 50/51, when it was robotically shifted from Node 3's port to Node 2's (Harmony) zenith port, supported by three U.S. extravehicular activities (EVAs) on March 24 (EVA 40), March 30 (EVA 41), and April 6 (EVA 42). These EVAs, involving astronauts Thomas Pesquet and Shane Kimbrough, reconfigured electrical connections, removed covers, and secured the adapter in its new position to prepare the zenith port for commercial crew vehicle operations. In 2019, PMA-3 at Harmony's zenith port was outfitted with the International Docking Adapter-3 (IDA-3), delivered by the SpaceX CRS-18 mission on July 25 and installed during U.S. EVA 55 on August 21 by astronauts Andrew Morgan and Nick Hague. The installation included attaching hemispherical reflectors, multi-layer insulation, and a planar reflector cover, enabling automated docking for future commercial spacecraft such as Boeing's Starliner and SpaceX's Crew Dragon. Maintenance of PMA-3 involves routine inspections during station operations to ensure structural integrity and functionality, given its role in supporting commercial vehicle dockings. Its zenith position on Harmony exposes it to increased risks from orbital debris compared to more sheltered locations, necessitating vigilant monitoring and protective measures. As of November 2025, PMA-3 remains at Harmony's zenith port with IDA-3 installed and operational.

References

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