Initial design specifications According to
Lew Allen, the initial key design elements were specified by
Edwin H. Land. They included i) solid state focal plane array, ii) integrated circuits for complex data processing, iii) large, fast optics with a diameter f/2 primary mirror, iv) gigabit/s data link, v) long on-orbit operational lifetime for the imaging satellites, and vi) communication satellites to facilitate close-to-realtime downlink of the images. A
NASA history of the Hubble, in discussing the reasons for switching from a 3-meter main mirror to a design, states: "In addition, changing to a 2.4-meter mirror would lessen fabrication costs by using manufacturing technologies developed for military spy satellites". Different versions of the KH-11 vary in mass. Early KH-11s were reported to be comparable in mass to HEXAGON, i.e. about . Later blocks are believed to have a mass of around to .
Optical Telescope Assembly A
CIA history states that the primary mirror on the first KH-11s measured , but sizes increased in later versions. Later satellites had larger mirrors, with a diameter of around . The focal plane was equipped with an array of light-sensitive silicon diodes, which converted brightness values to electrical signals. The packaging density was sufficiently high (several hundred diodes per inch) to match the ground sample distance of the
CORONA satellites. The recorded digital signal was encrypted and transmitted to a ground station in near real time, and written to film by means of a laser in order to recreate the recorded image. The first
charge-coupled device (CCD) detectors for KH-11 were developed by
Westinghouse Electric Corporation at their Baltimore facility in the later 1970s. KH-11 Block II might have been the first reconnaissance satellite equipped for imaging with an CCD. Later block satellites may include
signals intelligence capabilities and greater sensitivity in broader
light spectrums (probably into
infrared). One of the initial on-orbit challenges were failures of the
Traveling-wave tubes, which amplified the communications signals sent from the imaging satellite to the relay satellites, and from the relay satellites to the ground stations. During crossings of the
ionosphere, ions could build up on the outside of the tubes, which were operated at 14,000 volts. This resulted in repeated sparking and deposition of carbon traces inside the tubes, ultimately shorting them out. The issue could be abated by changing the orbiting satellite's orientation during crossing of the ionosphere, and was finally solved by better shielding of the tubes in follow-up satellites.
Resolution and ground sample distance A perfect
mirror observing in the visual spectrum (i.e. at a wavelength of 500 nm) has a
diffraction limited resolution of around 0.05
arcsec, which from an orbital altitude of corresponds to a
ground sample distance of .
Operational resolution should be worse due to effects of the
atmospheric turbulence. Astronomer
Clifford Stoll estimates that such a telescope could resolve up to "a couple inches. Not quite good enough to recognize a face".
KH-11 generations Five generations of U.S. electro-optical reconnaissance have been identified:
Block I Block I refer to the original KH-11 satellite, of which five were launched between 19 December 1976 and 17 November 1982.
Block II The three Block II satellites are in the open literature referred to as KH-11B, the alleged
DRAGON codename, or
CRYSTAL, and are believed to be capable of taking infrared images in addition to optical observations. Another improvement was an eightfold increase in the download rate compared to earlier models to facilitate improved real-time access and increased area coverage. From Block III on, the typical lifetime of the satellites increased to about 15 years, possibly related to a higher lift-off mass, which facilitates larger fuel reserves for countering atmospheric drag.
Block IV Three electro-optical satellites launched in October 2005, January 2011, and August 2013 are attributed to Block IV.
Block V A new generation of clandestine communications satellites launched to inclined geosynchronous orbits have led to speculations that these are in support of Block V electro-optical satellites scheduled for launch in late 2018 (NROL-71) and 2021 (NROL-82).{{cite web|title=Spy satellite infrastructure supported by successful Atlas V rocket launch|date=28 July 2016|first=Justin|last=Ray|publisher=Spaceflight Now Based on the published hazard areas for the launch, an orbital inclination of 74° has been deduced for NROL-71. This could indicate that NROL-71 is targeted for a
Type II Multi Sun-Synchronous Orbit,{{cite web|title=On Sun-Synchronous Orbits and Associated Constellations|date=7 December 2018|first=Daniele|last=Mortari|publisher=cranfield.ac.uk == Derivatives ==