visibility Similar

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code Related

41D-101-002 - STS-41D - Hardware attached to edge of SAE panel during OAST-1 experiment

description

Summary

The original finding aid described this as:

Description: Photographic documentation showing hardware attached to the edge of the extended Solar Array Experiment (SAE) panel during the Office of Aero. and Space Technology 1 (OAST-1) experiment in the payload bay of the orbiter Discovery during STS-41D.

Subject Terms: SOLAR ARRAYS HARDWARE SPACEBORNE EXPERIMENTS SPACE SHUTTLE MISSION 41-D DISCOVERY (ORBITER)

Categories: Payloads

Interior_Exterior: Exterior

Ground_Orbit: On-orbit

Element: Shuttle Payload Bay

Original: Film - 35MM CN

Preservation File Format: TIFF

STS-41D

Nothing Found.

label_outline

Tags

hardware edge sae panel sae panel oast experiment nasa solar array spaceborne experiments sts 41 d discovery payload bay high resolution solar arrays hardware spaceborne experiments space shuttle mission sts 41 d solar array experiment shuttle payload bay oast 1 experiment tiff sts 41 d orbiter discovery space technology payloads oast 1 orbiter discovery space program 1980 s us national archives
date_range

Date

1981 - 1989
create

Source

The U.S. National Archives
link

Link

https://catalog.archives.gov/
copyright

Copyright info

No known copyright restrictions

label_outline Explore Sae Panel, Solar Arrays Hardware Spaceborne Experiments Space Shuttle Mission, Solar Array Experiment

41D-37-093 - STS-41D - OAST-1 payload in the Discovery's payload bay

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the background, Paul Ogletree observes the monitor. Attached to the leading edge of the wing of the orbiters, the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

41D-101-061 - STS-41D - Hardware attached to edge of SAE panel during OAST-1 experiment

STS062-06-008 - STS-062 - View of OAST-2 in payload bay from window

41D-35-092 - STS-41D - Solar array panels for the OAST-1 payload

41D-101-017 - STS-41D - Hardware attached to edge of SAE panel during OAST-1 experiment

41D-38-057 - STS-41D - Solar arrays for the OAST-1 payload

41D-35-090 - STS-41D - Solar array panels for the OAST-1 payload

US Air Force (USAF) AIRMAN First Class (A1C) Adam Hooke, Hydraulic Journeyman, Accessories flight, 31st Maintenance Squadron (MXS), sets up the AvTec 843 Hydraulic Test Stand. This operation checks hydraulic equipment on the F-16 Fighting Falcon to include; Brakes, shocks, flight controls - such as leading edge slats. The test stand insures the equipment generates and handles the proper hydraulic pressure

OAST OFFICE OF AERONAUTICS AND SPACE TECHNOLOGY SPACE PROPULSION EXHIBIT

41D-37-108 - STS-41D - Solar arrays for the OAST-1 payload

41D-102-041 - STS-41D - Hardware attached to edge of SAE panel during OAST-1 experiment

Topics

hardware edge sae panel sae panel oast experiment nasa solar array spaceborne experiments sts 41 d discovery payload bay high resolution solar arrays hardware spaceborne experiments space shuttle mission sts 41 d solar array experiment shuttle payload bay oast 1 experiment tiff sts 41 d orbiter discovery space technology payloads oast 1 orbiter discovery space program 1980 s us national archives