NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Engineering Design of the Orbiting Astronomical ObservatoryThe Orbiting Astronomical Observatory (OAO) is designed to provide an accurately stabilized, unmanned platform for astronomical observations from well above the earth's atmosphere. Of primary immediate interest is the observation of stellar radiation in the ultraviolet range, which is severely limited even in balloon experiments because of absorption in the ozone layers. The OAO is a 3600-pound spacecraft that will be placed in orbit by an Atlas Agena D. It can handle optical systems up to 48 inches in diameter, 10 feet in length, weighing 1000 pounds. The key design requirements of the spacecraft are discussed. The reasons behind the configuration are then explained, followed by a discussion of the major subsystems showing how they have been designed to meet the exacting requirements astronomical observation.
Document ID
19630005296
Acquisition Source
Goddard Space Flight Center
Document Type
Contribution to a larger work
Authors
Walter H. Scott, Jr.
(Grumman Aircraft Engineering Corporation Bethpage, NY, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Publication Information
Publication: The Observatory Generation of Satellites Session Ii of A Special Astronautics Symposium Held at the Franklin Institute, Philadelphia, Dec. 27, 1962, During the 129th Annual Meeting of the American Association for the Advancement of Science
Publisher: National Aeronautics and Space Administration
Subject Category
Structural Mechanics
Accession Number
63N15172
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATELLITE INSTRUMENTATION
TEMPERATURE CONTROL
SATELLITE CONFIGURATION
SATELLITE ORIENTATION
OAO
OPTICAL INSTRUMENT
STABILITY AND CONTROL
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available