[Editor’s Note: this is the
first of a two-part article.]
In 1995 the Central
Intelligence Agency declassified the existence of the
CORONA series of reconnaissance satellites, which had
operated from 1960 until 1972. President Dwight D.
Eisenhower, who had approved the satellite’s development
in early 1958, was hailed by agency and military
officials as a visionary who had approved a
revolutionary intelligence collection system. But in
1960, after Gary Powers’ U-2 was shot down over the
Soviet Union and high-resolution photography of Soviet
targets ceased, Eisenhower approved a second
reconnaissance satellite named GAMBIT that was equally
revolutionary to the CORONA. GAMBIT produced
very-high-resolution photographs of Soviet military
installations until the last launch, in 1985. (Spy
satellite names were almost always printed in all-caps
in official documents.)
GAMBIT’s existence was
supposed to be declassified in 1998. The bureaucratic
paperwork was all signed and the last steps were being
taken to release the information. However, something
happened to prevent that. What is not exactly clear,
although the Indian nuclear tests in May 1998, and
evidence that the Indians may have deliberately hidden
their actions from American reconnaissance, may have
shifted the balance of the declassification argument in
favor of those who opposed any discussion of American
reconnaissance capabilities. In 2002, the US government
released imagery taken by the first GAMBIT satellites,
although it did not divulge any information about the
spacecraft, refusing to even admit that the National
Reconnaissance Office had launched them and in fact
never even mentioning the name “GAMBIT.”
Eight years of a secretive
Bush administration did not change the situation.
However, now that a new President is about to take
office, there is a possibility that secrecy rules may be
loosened and the GAMBIT fully declassified. This was a
Cold War system using technology that the National
Reconnaissance Office officially declared obsolete over
a decade ago. Hopefully, its contribution to American
national security and international stability may now be
told.
Despite the secrecy,
significant details of GAMBIT’s history have already
been revealed, both in documents and interviews
conducted over the past several years. This two-part
article is an abridged version of a series on American
satellite reconnaissance that will probably appear in
the British Interplanetary Society’s magazine Spaceflight later
this year.
Secret satellite
The United States flew
approximately two dozen U-2 aerial reconnaissance
missions over the Soviet Union between 1956 and 1960
when Francis Gary Powers was knocked out of the air by
an SA-2 missile. The U-2 produced beautiful photographs
of its targets, regularly achieving ground resolution of
two feet (0.6 meters) or better. But when it was no
longer able to fly over “denied territory”, the American
intelligence community needed a replacement. President
Dwight D. Eisenhower approved one in August 1960. It was
named GAMBIT.
Now
that a new President is about to take office,
there is a possibility that secrecy rules may be
loosened and the GAMBIT fully declassified.
Hopefully, its contribution to American national
security and international stability may now be
told. |
When the new satellite
project was first under discussion in the senior levels
of the US government in early 1960, presidential science
advisory George Kistiakowsky expressed his concern over
the military’s ability to operate a covert program. The
CIA had developed the highly successful U-2 spyplane and
was then developing the CORONA reconnaissance satellite.
But according to one source, the CIA “had no interest”
in expanding its role to include developing this new
reconnaissance system.
Air Force Under Secretary
Joseph Charyk strongly argued that the new program
should be developed by the Air Force. He stated that he
could prove that the Air Force could develop a covert
satellite. In the summer of 1960 Charyk and Colonel John
L. Martin, Jr. invented a new security strategy called
“Raincoat” that would be used to shield the covert
development program. Raincoat worked by classifying all military
space programs. The plan was that with everything
classified, it would be harder for outsiders to detect
the presence of a new reconnaissance satellite project.
According to one source, at
first this project was known only as “Program I”.
Sometime soon after the project gained formal approval,
it was given the secret code-name designation GAMBIT.
The origins of the name are still classified, but the
satellite was a gamble, for it involved new and
revolutionary technology. Perhaps equally risky, the
White House gave management authority for the project to
the Air Force, which by summer 1960 was under
considerable criticism for its management of the Samos
reconnaissance program.
In contrast to the
publicity surrounding its counterpart, the Samos E-6
search satellite that was started at the same time, the
covert effort to build GAMBIT did not leak to the press
during the next several years. Dozens of people had sat
in on a National Security Council meeting that gave a
stamp of approval to the E-6. Probably no more than a
handful of people were present when Eisenhower approved
GAMBIT. The results were readily apparent on the pages
of national magazines like Aviation
Week—often referred to as “Aviation Leak,” where
GAMBIT never appeared.
A new type of intelligence
When CORONA was started in
early 1958 its purpose had been to develop the best
reconnaissance camera in the shortest possible period of
time. Initially CORONA was described as an “interim”
system until something better came along. But its
photographs could only show large objects such as
buildings and airfields. GAMBIT’s resolution would be
much higher and its purpose was “technical
intelligence”, which meant the gathering of technical
data about its targets. For instance, it was one thing
to spot a missile site on the ground in the Soviet
Union. However, if a satellite could provide a
high-resolution photograph of an ICBM silo under
construction it would be possible to measure the
thickness of its concrete walls and determine how close
an American nuclear warhead would have to strike to
breach those walls.
The value of
high-resolution reconnaissance photos was not simply the
detail that they showed, but how they contributed to an
overall understanding of what was happening on the
ground. High-resolution photos enhanced the value of
low-resolution photos. For instance, high-resolution U-2
photographs could be used to identify objects that were
only blobs in CORONA photos. Similarly, after the United
States flew low-level reconnaissance missions over
missile sites in Cuba during the 1962 missile crisis,
photo-interpreters were able to look at CORONA
photographs of similar missile sites in the Soviet Union
and identify blurry objects, which the aircraft photos
revealed to be things like trucks, trailers, or tool
sheds.
GAMBIT was intended to
replace the U-2’s technical intelligence capabilities.
Technical intelligence required high resolution. In
order for GAMBIT to achieve it, the satellite had to
carry a large camera that achieved its power both
through brute force and ingenuity.
The
U-2 spy plane. The KH-7 GAMBIT was intended
to replace the U-2 in the dangerous job of
producing high-resolution photographs of the
Soviet Union. (credit: NASA)
|
A powerful telescope in
orbit
GAMBIT was started after
Eastman Kodak Company of Rochester, New York suggested
adapting a high-power camera system that the company had
apparently originally proposed for another purpose,
probably an aerial reconnaissance camera for use in an
RB-57 spyplane. Kodak’s design for the GAMBIT camera was
bold, almost radical. The company’s engineers combined a
reflecting telescope design and a film exposure
technique known as a strip camera to achieve very high
resolution.
Reflecting telescopes had
been around for hundreds of years, particularly in
ground-based astronomy. Extremely large and heavy
mirrors had been used for decades. For instance, a
100-inch (254-centimeter) mirror telescope entered
operation on top of Mount Wilson in 1917. The famed
Palomar Telescope in California, built in 1948, had a
mirror diameter of 200 inches (508 centimeters).
Kodak’s
design for the GAMBIT camera was bold, almost
radical. The company’s engineers combined a
reflecting telescope design and a film exposure
technique known as a strip camera to achieve
very high resolution. |
The design that Kodak
proposed for GAMBIT in early 1960 was a compound mirror,
meaning that more than one mirror was used to focus the
image on the film. A large curved “primary” mirror with
a hole in its center—like a donut—was located at the
base of the telescope and a smaller “secondary” mirror
was fitted in front of it. Light would enter the
aperture, bounce off the primary mirror, which would
focus it on the secondary mirror, which would then
bounce it back through the hole in the primary mirror
through a long thin exposure slit, where it would strike
a platform at the camera’s focal point known as a
platen. The platen held the film in place during
exposure.
Because the light was
folded inside the telescope, it could be shorter than a
similarly powerful telescope using conventional lenses
to focus the light down a long tube. It would be wider
than such a telescope, but another advantage was that
only a few mirrors were required and they could be made
lighter than the many thick and heavy glass lenses used
in a conventional telescope system.
Compound mirror designs
were popular for ground-based telescopes but rare in
most other applications. The military has used them for
some purposes, such as weapons sighting systems and
sniper rifles. They briefly became popular among
photographers during the 1950s as lightweight telephoto
lenses that did not extend far out in front of the
camera and therefore made the cameras easier to carry
and store.
But engineering is always
about compromises, and there was an obstacle to applying
this design to satellites that Kodak’s designers had to
overcome. Because the mirror arrangement was large and
relatively thick, they could not point it straight out
of the side of the spacecraft. Normally a solution would
be to point it straight out of the nose of the
spacecraft and point that down toward the Earth; this
was the approach used by the unsuccessful Samos E-1 and
E-2 film-readout satellites. However, the new camera
used conventional film that had to be returned to Earth
in a reentry vehicle mounted on the nose of the
spacecraft. So what the camera designers did was to
mount a third mirror, known as the image-reflecting
mirror, in front of the other mirrors. This
image-reflecting mirror looked out through a camera port
in the side of the spacecraft down at the Earth. It
reflected the vertical light from the Earth horizontally
and onto the primary mirror, the same way a submarine
periscope reflects horizontal light down a vertical
tube.
This image-reflecting
mirror had to tilt forward and back. This enabled it to
reflect images at different angles, probably a total of
30 degrees difference, providing a stereo capability
that allowed the photographic analysts to measure the
size of ground objects.
Even though reflecting
telescopes had existed for decades, adapting them for
spaceflight presented many challenges. The primary
technical challenge facing the designers was making the
mirrors relatively lightweight. Ground-based telescope
mirrors were made of polished glass and weighed tons. In
fact, they were deliberately heavy in order to
counteract the gravity that distorted their shape and to
reduce vibration. Mirrors for satellites had to be much
lighter and made of special materials. The details of
how Kodak’s engineers made the GAMBIT mirrors
lightweight remain classified. One person who was
involved with the GAMBIT program remembered that Kodak
used quartz for its mirrors, which was not the lightest
material then in development for satellite use.
Beryllium was ideal, but it was hazardous to work with.
The primary mirror on the
GAMBIT camera had a 44-inch (112-centimeter) diameter
that filled up much of the 60-inch (152-centimeter)
diameter of the payload cylinder that housed it.
Overall, the camera had a 77-inch (196-centimeter) focal
length, the distance from the point where light enters
the camera—the surface of the primary mirror—to the
point where it was focused, the film platen. As with all
long focal length precision optics, temperature had to
be precisely controlled. A small temperature increase
would cause the camera materials to expand or contract,
moving the mirrors out of focus. Camera designers for
other cameras controlled temperature in a number of
ways, including careful selection of materials with
known temperature response, passive thermal control of
the spacecraft environment through the use of shades and
reflective paints, and the addition of small heaters at
key parts of the camera.
The GAMBIT camera was the
first time that a spacecraft employed a reflecting
mirror telescope to focus the light, which was
undoubtedly challenging. But the design was also
revolutionary for another reason, the clever way that
the camera actually exposed the film.
Elegance in motion
Powerful reconnaissance
cameras have never really operated in the way that
conventional commercial cameras do. A 35-millimeter
single lens reflex (SLR) camera like those used by
professional photographers works by opening a shutter to
simultaneously expose the entire area of a rectangular
piece of film. In contrast, many of the early
reconnaissance satellite cameras developed by the United
States did not expose a rectangular frame, but rather a
long thin slit, taking advantage of the fact that the
image at the center of a lens is sharper than the image
near the edges, and covering much more territory.
Kodak’s
design for the GAMBIT camera was bold, almost
radical. The company’s engineers combined a
reflecting telescope design and a film exposure
technique known as a strip camera to achieve
very high resolution. |
In the case of the CORONA,
the camera itself rotated, and the aperture, a narrow
slit, was swept over a stationary piece of film,
producing a long thin image during a period of several
seconds. The CORONA camera design, first conceived in
the mid-1950s, was advanced for its day, but also
awkward. The tube, or “cell,” carrying the camera lenses
had to be rotated. The lenses were heavy and rotating
the cell produced vibrations. One Lockheed technician
remembered that testing the CORONA camera system on the
ground prior to flight produced a tremendous amount of
noise, a clackety-clack sound that led them to force all
people without the required security clearance to leave
the building so they would not suspect what the payload
was.
For GAMBIT, Eastman Kodak’s
engineers proposed an entirely different way to expose
the film known as the strip exposure technique. Strip
cameras had first been invented in the 1930s by camera
and reconnaissance designer George Goddard. Goddard was
in many ways the father of American aerial
reconnaissance and significantly advanced reconnaissance
technology during World War II.
Goddard had the idea of
pulling the film through the camera at the same speed
that the camera was moving and exposing it along a thin
vertical slit. The result was that the camera exposed a
long strip of film. He initially used it to photograph
racehorses at the finish line, where the racehorses
appeared sharp and crisp.
Goddard realized that his
strip camera could be valuable for aerial
reconnaissance, where the platform was constantly
moving. Normally the moving platform produces a slightly
blurred image because the image moves inside the camera
while the film is being exposed. But Goddard determined
that if he could move the film at the same speed as the
image moved inside the camera, the movements would
cancel each other out and there would be no blurring. He
employed this for reconnaissance planes during World War
II, where the biggest problem was getting the pilots to
fly an exact speed when they turned on their cameras.
Compared to an airplane, a
satellite was an ideal platform, because the satellite
would travel at a constant rate of speed in its orbit.
The primary problem would be precisely determining that
rate of speed. The designers would not know exactly what
orbit the rocket would place the satellite in, but once
it was safely in orbit they could track it from the
ground and adjust the camera so that it pulled the film
past the exposure slit at a precise rate of speed.
The result was a camera
that had fewer moving parts and less vibration than the
CORONA. Pulling film through a powerful camera was a
much more elegant solution than rotating a heavy lens
cell past a long strip of film.
The GAMBIT camera used
nine-inch-wide (23-centimeter-wide) film, over three
times the width of the 70-millimeter film employed in
the CORONA camera. Nine-inch film was a typical size for
large-format aerial reconnaissance cameras. The film did
not have sprockets on its edge and was pulled through
the camera by tension from the takeup wheel. The camera
only exposed about 8.5 inches of the film width, leaving
thin strips on either side for recording camera data,
such as the reconnaissance mission number, the date and
time, and the frame. This data was projected onto the
film by small diodes mounted inside the camera.
There is a basic rule of
optics that the more powerful the magnification, the
smaller the field of view. This inevitable tradeoff also
applies to reconnaissance satellites. GAMBIT had a
powerful camera that could only focus upon a small bit
of territory on the ground. From a normal orbit of 90
nautical miles (167 kilometers), the camera would see a
strip approximately 12 nautical miles (22 kilometers)
wide. However, the strip camera had one partial
advantage, which was that it could expose new film as
long as the shutter was open. So although the film
imaged the ground 12 miles wide, there was virtually no
limit to how long an image it could take. In practice,
the KH-7 GAMBIT camera could take strips that were as
short as 5 nautical miles and as long as 400 nautical
miles (741 kilometers), although most strips were about
twice as long as they were wide. The vast majority of
ground targets could fit in such a strip.
There was one other
limitation on how much the camera could photograph.
Because the satellite used the same camera to take
photos from different angles, if programmers wanted
stereo photographs of a target they would have to turn
on the camera, take a photo for a short strip, and then
close the exposure slit, move the image reflecting
mirror to its new position, and then open the slit again
to expose a new piece of film. Other targets could be
missed while the camera was doing all of this. In
addition, starting and stopping the film meant that
occasionally the image smeared a bit at the leading edge
as the film accelerated from zero speed to the speed of
the image through the camera. Operators could compensate
for this by starting the camera before reaching the
target, which wasted a small amount of film but ensured
that the target would be sharp.
KH-7
reconnaissance satellite image. (courtesy J.
Richelson)
|
Hawkeye’s spies in the sky
Eastman Kodak manufactured
the GAMBIT camera at its secretive Hawkeye facility in
Rochester, New York. Kodak manufactured and processed
the high-quality film used in aerial and satellite
reconnaissance cameras. The company also designed and
built various reconnaissance cameras such as the Samos
E-1, E-2, E-6, and GAMBIT. Kodak is not publicly known
as a major defense contractor, and the company’s
leadership prefers it that way. Even today Kodak’s
former executives and employees remain tight-lipped
about their role in developing some of the most powerful
reconnaissance cameras ever built.
One young Air Force officer
who traveled to view the GAMBIT camera manufacturing
facility at the Hawkeye plant in the late 1960s
remembered walking through a large cleanroom where
dozens of women were assembling small commercial
cameras. Because of the requirement for dust-free
operations the women wore nothing under their white
jumpsuits. The officer fondly remembered that the women
occasionally flashed their bare chests at the Air Force
visitors, which made the visit to cold Rochester
worthwhile.
Hilliard Page, an executive
at General Electric, the company responsible for the
manufacture of the GAMBIT spacecraft and its reentry
vehicle, remembered that dealing with the Kodak
engineers was a lot different than dealing with the
engineers at Itek, which manufactured the CORONA camera.
Itek was a small, entrepreneurial firm that needed all
the business it could get. Kodak was a massive,
profitable corporation that did not really need the
reconnaissance business. Its engineers were self-assured
to the point of arrogance, and told Paige that everyone
would do things their way or not do them at all.
Ellis Lapin, an engineer at
The Aerospace Corporation who worked on GAMBIT from 1962
until 1966, remembered that his boss found Kodak
difficult to deal with, but Lapin himself never
experienced this. “In my own dealings with high level
management and with the engineers at Kodak,” Lapin
wrote, “I found the former deferential to a degree that
surprised me and the latter cooperative and intent on
doing a good job.”
Samos E-6 search
satellite. The E-6 was intended to replace the
CORONA and accompany the KH-7 GAMBIT; the E-6 would
find the targets and the GAMBIT would photograph
them close up. But the E-6 was unsuccessful. The
camera for the E-6, like the camera for GAMBIT, was
built by Eastman Kodak. (credit: NRO)
The bang-bang OCV
GAMBIT was started at
the same time as the Air Force Samos E-6 search
satellite that was intended to replace the CIA’s
CORONA. In summer 1960 Air Force Undersecretary
Joseph Charyk forbid Lockheed from competing to
build the E-6 spacecraft in order to spread the work
around and expand the industrial base for
manufacturing reconnaissance satellites. At the time
Lockheed already had a virtual monopoly on the
manufacture of Air Force satellites. Air Force
officials felt that the company was overbooked and
were also unhappy with its performance on the CORONA
program, which had suffered a string of failures.
From Charyk’s viewpoint it made sense to broaden the
satellite industrial base by giving contracts to
other aerospace companies.
It is highly likely
that Lockheed was also forbidden from competing to
build the GAMBIT spacecraft. The same company that
won the Samos E-6 spacecraft contract, General
Electric, also won the contract to build the GAMBIT
spacecraft. General Electric manufactured the
Orbital Control Vehicle, or OCV, for the GAMBIT
program. CORONA used Lockheed’s Agena upper stage to
provide power and stability in orbit. GAMBIT would
still require an Agena to reach orbit, but it would
discard it and rely upon the OCV for highly precise
pointing and overall stability.
It
is highly likely that Lockheed was also
forbidden from competing to build the GAMBIT
spacecraft. The same company that won the
Samos E-6 spacecraft contract, General
Electric, also won the contract to build the
GAMBIT spacecraft. |
The OCV was a squat
cylinder 60 inches in diameter, the same diameter as
the Lockheed Agena upper stage that boosted it to
orbit. It contained horizon sensors for accurately
orienting the spacecraft, and a cold gas control
system—sometimes called a “bang bang system” because
it would fire bursts from its jets in quick
pulses—to stabilize and point the spacecraft in its
orbit. These systems were important because the
camera’s field of view was so small that it might
point in the wrong direction and miss its target.
This was one of the driving factors behind Director
of Central Intelligence John McCone’s support of the
KH-6 LANYARD satellite. LANYARD was started a year
after the GAMBIT, in December 1961. It utilized the
camera system from the Samos E-5, which had suffered
several spacecraft failures. The CIA had started
LANYARD to serve as an interim system until GAMBIT
became operational. But McCone also viewed the
LANYARD as “insurance” in case GAMBIT experienced
problems.
The primary factor that
affected any reconnaissance spacecraft’s pointing
capabilities was moving mass inside the vehicle. Any
moving mass could cause the spacecraft to move in
the opposite direction. The major source of movement
in the spacecraft was the camera system, and there
were several parts of the GAMBIT camera that moved.
The image reflecting mirror pitched back and forth
to provide stereo photographs by changing the angle
that light entered the aperture. However, the
biggest source of movement was the film spools: the
supply spool in the rear of the spacecraft and the
takeup spool in the nose that collected the exposed
film. They would impart a pitching movement on the
spacecraft as they started and stopped. GAMBIT’s
designers reduced the effects of this by looping
some of the unexposed film back and forth before it
went to the platen. That way the film could be drawn
through the camera without having to turn the heavy
spools at the same time the camera was exposing
film. But the Orbital Control Vehicle’s cold gas
stabilization system had to quickly dampen any
movement as a result of camera operation.
At some point early in
the GAMBIT’s development program managers made an
important decision concerning its reentry vehicle.
They decided to use the same reentry vehicle
developed by General Electric for the CORONA
program. Publicly this was known as the Discoverer
Satellite Recovery Vehicle, or SRV, after the
Discoverer cover story developed for CORONA.
Although the SRV was relatively small, it had the
virtue of being proven.
This decision had
drawbacks, however. The GAMBIT’s film was over three
times as wide as CORONA’s, but had to be stuffed
into the same amount of space. It is unknown if the
limiting factor for how much film the GAMBIT could
carry was weight or volume. Eventually the CORONA
SRV would carry two spools of ultra-thin film each
16,000 feet (4,877 meters) long and weighing 160
pounds (73 kilograms) total. The GAMBIT SRV carried
a maximum of only 3,000 feet (914 meters), roughly
equivalent in weight to 9,000 feet (2,743 meters) of
CORONA film, so the limiting factor was probably the
volume of the wider film in the SRV rather than its
weight.
Another limitation of
the CORONA SRV was reentry accuracy. The vehicle did
most of its slowing down in the upper atmosphere,
following a shallow trajectory. As a result, its
reentry “footprint” could be quite large, extending
30 nautical miles (56 kilometers) to either side of
its ground track and up to 200 miles (370
kilometers) long. Because its footprint was so
large, many more aircraft had to be spread out over
a much larger area to retrieve it. In fact, at the
time that program managers chose the conservative
option of using the CORONA SRV, General Electric was
already working on developing a larger and more
accurate SRV for the Samos E-6 satellite to reduce
this footprint. They were also exploring the
possibility of developing a lifting body reentry
vehicle that could land inside the United States
carrying reconnaissance film.
Although the Discoverer
SRV had limitations, the program managers eventually
realized that they had made the right decision to
use a proven design. CORONA capsules returned from
orbit regularly, but other Air Force efforts to
develop larger and more precise reentry vehicles
failed miserably.
Technology transfer was
not all one-way, however. GAMBIT’s designers
developed a backup battery system called “Lifeboat”
which insured de-orbit of the recovery vehicle in
event of spacecraft power failure. Lifeboat was soon
incorporated into the CORONA.
GAMBIT management
By September of 1961
the Secretary of Defense made several organizational
changes to clarify the management of satellite
reconnaissance projects. The Office of Missile and
Satellite Systems was renamed the National
Reconnaissance Office, or NRO. The Samos Program
Office was renamed the Office of Special Projects,
or OSP. The NRO was a secret agency and Joseph
Charyk was named its first director. Within the NRO
the Office of Special Projects’ secret designation
was Program A. Program A was responsible for
developing the GAMBIT and other satellites.
By March 1962 GAMBIT
was taken over by Colonel William G. King, who was
the most experienced Air Force officer in the
satellite reconnaissance field. He had taken over
the WS-117L reconnaissance satellite office in early
1956 and had served in that post until 1958 when he
was transferred to run the trouble-plagued Snark
cruise missile program.
As
GAMBIT progressed it suffered schedule
delays and cost overruns, but their nature,
severity, and cause remain unknown. |
In 1962 the NRO created
the KH series of designations for certain
reconnaissance satellites. KH stood for KEYHOLE,
which was the existing code word for the security
compartment covering satellite imagery. But the KH
designation was only assigned to covert satellite
programs, not to the pre-existing Samos camera
systems that were already public. GAMBIT was
assigned the designation KH-7.
GAMBIT also had another
designation that was probably applied in late 1961.
It was known as Air Force Program 206. This was an
unclassified designation used in official paperwork,
such as travel orders for Air Force personnel
working on the project.
As GAMBIT progressed it
suffered schedule delays and cost overruns, but
their nature, severity, and cause remain unknown.
The first KH-7 GAMBIT reconnaissance
satellite launch, July 1963. (Courtesy
Jonathan McDowell)
|
The folding Atlas
By early 1963 the
GAMBIT program was approaching its first launch,
scheduled for the summer. But in May 1963 an
Atlas-Agena D launch vehicle was on the pad at
Vandenberg Air Force Base undergoing tests. Atop the
Atlas was a non-operational payload simulating a
GAMBIT satellite. As space historian Joel Powell
recently wrote, this test ended in an embarrassing
accident.
During fueling a bubble
developed in the ground system pumping liquid oxygen
into the Atlas, knocking a valve out of alignment.
Ground crews then had to manually drain the liquid
oxygen tank. But the Atlas received its structural
strength from internal pressure. While the oxygen
was being drained the vehicle collapsed, crumpling
like an empty soda can and causing the Agena and its
payload to fold over and hit the pad nose first. A
surge of either fuel or residual liquid oxygen also
damaged the launch tower, which had to be repaired
before another Atlas could be launched.
The event was similar
to an early failure in the CORONA program before the
first launch, where a vehicle on the pad suffered a
catastrophic failure. That event had been labeled
“CORONA Zero,” and it had served as a wake-up call
to the program’s managers about the importance of
carefully checking all of the systems before the
vehicle ever reached the pad. In the case of the
crumpling Atlas in May 1963, although the Atlas was
a total loss, the Agena and its payload were
apparently only mockups, not flight hardware, and
the program recovered quickly from the accident.
A conservative start
The first GAMBIT
mission was launched on July 12, 1963. Its
Atlas-Agena lifted off its launch pad at Vandenberg
and headed south. The Atlas performed properly and
when it burned out it fell away. The Agena’s Bell
rocket engine then fired and pushed the payload into
polar orbit, at 102 miles (189 kilometers) altitude.
The mission was designated 4001.
An engineer at The
Aerospace Corporation had recommended that, during
GAMBIT’s first flights, the Orbital Control Vehicle
should remain attached to the Agena throughout the
flight. This was a confidence-building decision
because the Agena was proven whereas the OCV was
not. However, it meant that photographs could only
be taken of targets directly below the vehicle.
After the photographic phase of the mission was
completed the reentry vehicle separated and came
down over the ocean northwest of Hawaii, where it
was caught in mid-air by a C-130 aircraft. Its film
was then transported to Eastman Kodak in Rochester,
New York, where it was processed and copied and then
sent to Washington for analysis.
After the reentry
vehicle was jettisoned the engineering phase of the
mission began. The OCV was separated from the Agena
and put through a series of tests to determine its
stability and other characteristics. Its performance
during these tests is unknown, but it did not
totally silence GAMBIT’s skeptics, particularly in
the CIA.
On September 6, 1963
the Air Force launched the second GAMBIT spacecraft
on mission 4002. Like its predecessor, this GAMBIT
also kept the Agena attached throughout the
photographic phase of the mission and then detached
for engineering tests after the reentry capsule had
returned to Earth. The mission also was successful.
Even after the second
GAMBIT launch, Albert Wheelon, the CIA’s Director of
Science and Technology, expressed skepticism about
GAMBIT. “The major question mark in our minds at
this point is that the uncertainties involved in
establishing the location of a satellite in orbit,
combined with the small swath width delivered by the
G system, may make it extremely difficult for us to
have adequate assurance of covering the targets for
which high-resolution photography is required. It is
possible, therefore, that neither G nor L[ANYARD]
will meet our technical intelligence requirement,
and that we may have to develop a system with
greater swath width and less resolution than G but
smaller swath width and greater resolution than L
and [CORONA]. We may also find that we cannot
achieve a useable system yielding GAMBIT’s ground
resolution from satellite vehicles.”
The third GAMBIT
mission, number 4003, was launched on October 25,
1963 and was also successful. The Agena again
remained attached. The film was ejected after the
photographic phase and the capsule recovered. The
OCV was then put through various tests once the
intelligence goals had been achieved.
GAMBIT operations and
problems
GAMBIT mission 4004 was
launched on December 18, and for the first time the
OCV and its payload detached from the Agena to
conduct the photographic phase of the mission. It
was successful, and the capsule was recovered the
next day.
Even after the second GAMBIT launch, Albert
Wheelon, the CIA’s Director of Science and
Technology, expressed skepticism about
GAMBIT. |
Four successful GAMBIT
missions in a row proved that the Air Force could
run a black satellite program that would work, and
the GAMBIT was a powerful new intelligence tool. But
CIA officials still complained. As John McMahon, an
official in the CIA’s Directorate of Science and
Technology, noted in a May 1964 memo, “In 1963 there
were four GAMBIT launches. Total target coverage
numbered only 15.” The CIA wanted to see GAMBIT’s
intelligence return increase substantially, and
fast.
By 1964 the KH-7 GAMBIT
quickly shifted into high gear. After only four
missions in the second half of 1963, the Air Force
launched ten GAMBITs in 1964, but not without
incident. In May 1964 mission 4008 suffered problems
when its Agena lost roll control during the boost
phase. The OCV also suffered system problems, but
the mission was still able to return some imagery.
But late in the year
the GAMBIT program suffered from major problems. In
October 1964 a GAMBIT mission failed to achieve
orbit when its Agena malfunctioned during launch.
Two weeks later mission 4013 achieved orbit, but for
unknown reasons returned no film. Ellis Lapin did
not remember the specific cause of the problem, but
thought that it might have been with the command
system. “In those days we used wire-recorders for
storing commands, and we did have problems with
them. Tape recorders were not yet in vogue,” he
explained.
The next mission, 4014,
was launched in early December, but suffered a
battery failure. “That failure was an explosion!”
Lapin exclaimed. Something in the batteries had
failed catastrophically and it required much effort
to find the cause and fix it.
In January 1965
Brockway McMillan, the Director of National
Reconnaissance, decided to delay plans to improve
the launch readiness of GAMBIT until after its
reliability problems had been solved. Mission 4019,
launched in June 1965, and mission 4020, launched in
July 1965, both apparently failed to return imagery.
Similarly, mission 4023 returned few images and
4034, launched in November 1966, returned no
imagery. Many years later retired General Electric
executive Hill Paige remembered that after the
program had experienced a string of successful
missions it suddenly suffered a number of
malfunctions—possibly the slew of failures in 1964
and 1965. Paige explained that this had ultimately
been traced to a change in the launch pad tower at
Vandenberg Air Force Base. An additional structure
had been added to the top of the tower and this had
reflected acoustic energy back on the vehicle during
launch, shaking loose components in the spacecraft.
Despite the problems,
the KH-7 GAMBIT was dramatically improving the
quality of American intelligence collection. But
intelligence officials wanted better results, and
they would get them with a major upgrade of the
spacecraft and camera system.
[Next: The
development of the KH-8 GAMBIT, FROG, HIGHER BOY,
and photographing Skylab from orbit.]
Dwayne Day is preparing
a series of articles on post-CORONA reconnaissance
satellites during the Cold War. These will cover the
Samos E-5 and E-6 satellites as well as the KH-6
LANYARD, KH-7 and 8 GAMBIT, and other proposals such
as SPARTAN. He can be reached at zirconic1@cox.net.