File:STS052-80-027 - STS-052 - STS-52 deployment of LAGEOS-IRIS spacecraft from OV-102's payload bay - DPLA - 2c81b2dbcf250811f310a003bad9c25e.jpg
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[edit]STS052-80-027 - STS-052 - STS-52 deployment of LAGEOS/IRIS spacecraft from OV-102's payload bay ( ) | ||||||||||||||||||||
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Creator InfoField | National Aeronautics and Space Administration. Lyndon B. Johnson Space Center. 2/17/1973 | |||||||||||||||||||
Title |
STS052-80-027 - STS-052 - STS-52 deployment of LAGEOS/IRIS spacecraft from OV-102's payload bay |
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Description |
The original finding aid described this as: Description: During STS-52 deployment activities, the Italian Research Interim Stage (IRIS), a spinning solid fuel rocket, lifts the Laser Geodynamic Satellite II (LAGEOS II) out of its support cradle and above the thermal shield aboard Columbia, Orbiter Vehicle (OV) 102. The remote manipulator system (RMS) arm, with Material Exposure in Low Earth Orbit (MELEO), is positioned above the port side sill longeron. On the mission-peculiar equipment support structure (MPESS) carriers in the center foreground is the United States (U.S.) Microgravity Payload 1 (USMP-1) with Space Acceleration Measurement System (SAMS), MEPHISTO (its French abbreviation), Lambda Point Experiment (LPE) cryostat assembly (identified by the JPL insignia), and LPE vacuum maintenance assembly. Other payload bay (PLB) experiments visible in this image include: on the starboard wall (left), the Canadian Experiments 2 (CANEX-2) Space Vision System (SVS) Canadian Target Assembly (CTA) (foreground) and the Attitude Sensor Package (ASP); and on the port wall (right), the Tank Pressure Control Experiment/Thermal Phenomena (TPCE/TP) get away special (GAS) canister. Subject Terms: STS-52, COLUMBIA (ORBITER), ARTIFICIAL SATELLITES, GEODYNAMICS, IRIS SATELLITES, GET AWAY SPECIALS (STS), ITALIAN SPACE PROGRAM, PAYLOAD BAY, PAYLOAD DEPLOYMENT & RETRIEVAL SYSTEM, REMOTE MANIPULATOR SYSTEM, SPACEBORNE EXPERIMENTS Date Taken: 10/23/1992 Categories: Payloads Interior_Exterior: Exterior Ground_Orbit: On-orbit Original: Film - 70MM CT Preservation File Format: TIFF feat: NON-EARTHOBS |
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Date |
23 October 1992 date QS:P571,+1992-10-23T00:00:00Z/11 |
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Collection |
institution QS:P195,Q59661040 |
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Source/Photographer |
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Permission (Reusing this file) |
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Standardized rights statement InfoField |
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This image or video was catalogued by Johnson Space Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: STS052-80-027. This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing. Other languages:
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Licensing
[edit]Public domainPublic domainfalsefalse |
This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) | ||
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current | 19:38, 23 November 2020 | 608 × 640 (42 KB) | DPLA bot (talk | contribs) | Uploading DPLA ID 2c81b2dbcf250811f310a003bad9c25e |
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author name string: National Aeronautics and Space Administration. Lyndon B. Johnson Space Center. 2/17/1973
Reference
STS052-80-027 - STS-052 - STS-52 deployment of LAGEOS/IRIS spacecraft from OV-102's payload bay (English)
Reference
Reference
Reference
Reference
The original finding aid described this as: Description: During STS-52 deployment activities, the Italian Research Interim Stage (IRIS), a spinning solid fuel rocket, lifts the Laser Geodynamic Satellite II (LAGEOS II) out of its support cradle and above the thermal shield aboard Columbia, Orbiter Vehicle (OV) 102. The remote manipulator system (RMS) arm, with Material Exposure in Low Earth Orbit (MELEO), is positioned above the port side sill longeron. On the mission-peculiar equipment support structure (MPESS) carriers in the center foreground is the United States (U.S.) Microgravity Payload 1 (USMP-1) with Space Acceleration Measurement System (SAMS), MEPHISTO (its French abbreviation), Lambda Point Experiment (LPE) cryostat assembly (identified by the JPL insignia), and LPE vacuum maintenance assembly. Other payload bay (PLB) experiments visible in this image include: on the starboard wall (left), the Canadian Experiments 2 (CANEX-2) Space Vision System (SVS) Canadian Target Assembly (CTA) (foreground) and the Attitude Sensor Package (ASP); and on the port wall (right), the Tank Pressure Control Experiment/Thermal Phenomena (TPCE/TP) get away special (GAS) canister. Subject Terms: STS-52, COLUMBIA (ORBITER), ARTIFICIAL SATELLITES, GEODYNAMICS, IRIS SATELLITES, GET AWAY SPECIALS (STS), ITALIAN SPACE PROGRAM, PAYLOAD BAY, PAYLOAD DEPLOYMENT & RETRIEVAL SYSTEM, REMOTE MANIPULATOR SYSTEM, SPACEBORNE EXPERIMENTS Date Taken: 10/23/1992 Categories: Payloads Interior_Exterior: E (English)
The original finding aid described this as: Description: During STS-52 deployment activities, the Italian Research Interim Stage (IRIS), a spinning solid fuel rocket, lifts the Laser Geodynamic Satellite II (LAGEOS II) out of its support cradle and above the thermal shield aboard Columbia, Orbiter Vehicle (OV) 102. The remote manipulator system (RMS) arm, with Material Exposure in Low Earth Orbit (MELEO), is positioned above the port side sill longeron. On the mission-peculiar equipment support structure (MPESS) carriers in the center foreground is the United States (U.S.) Microgravity Payload 1 (USMP-1) with Space Acceleration Measurement System (SAMS), MEPHISTO (its French abbreviation), Lambda Point Experiment (LPE) cryostat assembly (identified by the JPL insignia), and LPE vacuum maintenance assembly. Other payload bay (PLB) experiments visible in this image include: on the starboard wall (left), the Canadian Experiments 2 (CANEX-2) Space Vision System (SVS) Canadian Target Assembly (CTA) (foreground) and the Attitude Sensor Package (ASP); and on the port wall (right), the Tank Pressure Control Experiment/Thermal Phenomena (TPCE/TP) get away special (GAS) canister. Subject Terms: STS-52, COLUMBIA (ORBITER), ARTIFICIAL SATELLITES, GEODYNAMICS, IRIS SATELLITES, GET AWAY SPECIALS (STS), ITALIAN SPACE PROGRAM, PAYLOAD BAY, PAYLOAD DEPLOYMENT & RETRIEVAL SYSTEM, REMOTE MANIPULATOR SYSTEM, SPACEBORNE EXPERIMENTS Date Taken: 10/23/1992 Categories: Payloads Interior_Exterior: E (English)
The original finding aid described this as: Description: During STS-52 deployment activities, the Italian Research Interim Stage (IRIS), a spinning solid fuel rocket, lifts the Laser Geodynamic Satellite II (LAGEOS II) out of its support cradle and above the thermal shield aboard Columbia, Orbiter Vehicle (OV) 102. The remote manipulator system (RMS) arm, with Material Exposure in Low Earth Orbit (MELEO), is positioned above the port side sill longeron. On the mission-peculiar equipment support structure (MPESS) carriers in the center foreground is the United States (U.S.) Microgravity Payload 1 (USMP-1) with Space Acceleration Measurement System (SAMS), MEPHISTO (its French abbreviation), Lambda Point Experiment (LPE) cryostat assembly (identified by the JPL insignia), and LPE vacuum maintenance assembly. Other payload bay (PLB) experiments visible in this image include: on the starboard wall (left), the Canadian Experiments 2 (CANEX-2) Space Vision System (SVS) Canadian Target Assembly (CTA) (foreground) and the Attitude Sensor Package (ASP); and on the port wall (right), the Tank Pressure Control Experiment/Thermal Phenomena (TPCE/TP) get away special (GAS) canister. Subject Terms: STS-52, COLUMBIA (ORBITER), ARTIFICIAL SATELLITES, GEODYNAMICS, IRIS SATELLITES, GET AWAY SPECIALS (STS), ITALIAN SPACE PROGRAM, PAYLOAD BAY, PAYLOAD DEPLOYMENT & RETRIEVAL SYSTEM, REMOTE MANIPULATOR SYSTEM, SPACEBORNE EXPERIMENTS Date Taken: 10/23/1992 Categories: Payloads Interior_Exterior: E (English)
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Reference
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