The fixtures allowed the Space Shuttle'sCanadarm (also known as the Shuttle Remote Manipulator System, or SRMS) to safely grapple large objects (e.g. ISS components, or satellites e.g. HST).
The grapple fixtures are flat in appearance, with a central grapple pin topped with a sphere which the snares in the end of the arms latch on to. They use three "ramps" that help guide the robotic arm correctly onto the grapple fixture.[2]
The North American grapple fixture was developed at Spar Aerospace in the 1970s. Its invention is credited to Frank Mee, who also invented the Canadarmend effector for the Space Shuttle.[3] The Grapple Fixture design was further refined by Barrie Teb.[3]
The Flight-Releasable Grapple Fixture (FRGF) is the simplest variation of the North American grapple fixture, it allows only for grappling and does not have any electrical connectors.[4] Its use began early in the Space Shuttle program and was developed from the Flight Standard Grapple Fixture (FSGF) by allowing the Grapple Shaft to be installed during extravehicular activity (EVA).[5]
Unpiloted ships like the SpaceX Dragon, Orbital ATKCygnus and Japanese H-II Transfer Vehicle include a standard FRGF which is used by the Canadarm2 to grapple the capsule on approach to the International Space Station for berthing.[6] The fixture can have a maximum payload rating of 65,000 pounds or 30,000 kg.[7]Anorbital replacement unit may also have a grapple fixture.
The Latchable Grapple Fixture (LGF) allows for grappling and latching, intended to be used for longer‐term stowage on the Payload Orbital replacement unit Accommodation (POA) (greater than 3 weeks).[4] It does not have any electrical connectors.[4]
Electrical Flight Grapple Fixture and Electro Mechanical Grapple Fixture
[edit]Electrical Flight Grapple Fixture used on the Space Shuttle's boomElectro Mechanical Grapple Fixture used on Kibo's Small Fine Arm
The Electrical Flight Grapple Fixture (EFGF) allows for grappling.[7] It has a single electrical connection for data, power,[7] and video from cameras on the manipulators.[8] The electrical connection is compatible with the Shuttle Remote Manipulator System (also known as Canadarm1).
Kibo (ISS module) Remote Manipulator System (Japanese Experiment Module Remote Manipulator System) uses a similar grapple fixture, called Electro Mechanical Grapple Fixture (EMGF).[9]
The Power and Video Grapple Fixture (PVGF) allows for grappling and latching.[4] It has electrical connectors for data, video, and power.[4] The electrical connections are compatible with the Space Station Remote Manipulator System (also known as Canadarm2).
The Power Data Grapple Fixture (PDGF) allows for grappling and latching.[4] It has electrical connectors for data, video, and power; it is also the only North American grapple fixture that is replaceable on-orbit.[4] The electrical connections are compatible with the Space Station Remote Manipulator System (also known as Canadarm2).
It is used on the International Space Station (ISS). PDGFs can be "grappled" by the Canadarm2 robotic arm, in order to allow the arm to manipulate and power a grappled object, or be commanded by operators based inside the ISS. PDGFs located around much of the station provide connections for the arm. They have four rectangular connectors to transfer data, video and electrical power. During the penultimate Space Shuttle flight a PDGF was installed on the Zarya module to support Canadarm2 operations based from the Russian segment.[10]
Long Duration Exposure Facility (LDEF) had two. An FRGF and an active (rigidize sensing) grapple used to send an electronic signal to initiate the 19 experiments that had electrical systems.[12]
[edit]A grapple fixture used by the European Robotic Arm, located on the Rassvet Mini-Research Module 1 (MRM1) of the International Space Station. This fixture, along with others allows for the European Robotic Arm to grapple and move around the station.
Although the European Robotic Arm uses grapples to relocate in a similar fashion to Canadarm2, the grapple fixtures are not compatible with each other. This means the European arm can only work on the Russian segments of the station.[13]
May 2020 - Shipped to Baikonur for final processing[14]
^Kyle Baker; Eryn Culton; Jonathan Lang; Zachary Lewis; Robert Perez-Alemany; Alexa Rizzo; Brendon Smeresky; Anthony Starks; Joshua Teneyck; Jennifer Rhatigan; Marcello Romano (2019). "An updated re-entry analysis of the Hubble Space Telescope"(PDF). First Int'l. Orbital Debris Conf.: 2. Retrieved May 12, 2023.
This article incorporates text from this source, which is in the public domain.
