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Project Pluto – Nuclear RAMJET Engines


Background
Project Pluto was a United States government program to develop nuclear powered ramjet engines for use in cruise missiles. Two experimental engines were tested at the United States Department of Energy Nevada Test Site (NTS) in 1961 and 1964.

Below, you will find the declassified documents available thus far. More requests are open, and when documents are received, they will be added here.


Declassified Documents
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The Impact of the High Development Cost of Advanced Flight Propulsion Systems on Development Policy, October 1965 [75 Pages, 3.7MB] – A discussion of techniques for handling R and D funds to reduce the investment risk in implementing programs for new propulsion systems, particularly systems which are novel and advanced. To guide the funding management, relevant R and D activities are described in detail, followed by a discussion of criteria to be met before an engine qualifies for consideration.

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Nuclear Ramjet Propulsion System Applied Research and Advanced Technology (Project Pluto). Volume V. Propulsion System Test Planning and Ground Test Facility Studies, 15 February 1963 [92 Pages, 24.8MB] – Test planning studies in this report present the concept of test programs, their scope, test objectives, probable testing schedule, estimated number of test weeks and test runs, existing facilities which can be utilized, and test conditions. The schedule and test plans presented are based upon the program outlined in the Air Force Development/Plan for Pluto. Flight engine ground test facility criteria are updated to reflect the latest facility studies and test planning. The site selection core drilling program and underground air storage experiment are described.

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Nuclear Ramjet Propulsion System Applies Research and Advanced Technology (Project Pluto). Volume VI. Structural Materials Investigations, 15 February 1963 [163 Pages, 5.8MB] – This is the “best copy available.” Although hard to read, I would recommend downloading it, and zooming in on the document with Adobe Acrobat, to get a bit of an easier reading experience.

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Nuclear Ramjet Propulsion System Applied Research and Advanced Technology (Project Pluto). Volume VII. Propulsion System Design and Structural Analysis, 15 February 1963 [163 Pages, 39MB] – This volume contains the results of design, structures, and materials studies and structures component testing of a nuclear propulsion system in support of the Pluto reactor program. These studies include design concepts, structural analysis of steady state and dynamic loads, material evaluation, and recommended dynamic and structural test programs. The methods of analysis used have been outlined in each case for reference.

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Nuclear Ramjet Propulsion System Project Pluto, 30 January 1962 [382 Pages, 37.9MB] – Contents: Propulsion System Design and Analysis — Tory IIC design data, Performance analysis, Engine performance summary, Heat transfer and thermal stress analysis, Mechanical and structural design, Neutronics, Radiation analysis and shielding, Aerodynamic experiments, Structural experiments, and Materials investigations; Propulsion System Controls — General status, Control system analysis, Control system components, and Radiation effects Testing; Flight Engine Facility and Test Planning — Facility design studies, and Underground air storage experiment.

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Aircraft Nuclear Propulsion Systems. Project Pluto, 15 November 1959 [165 Pages, 123MB] – To provide accurate and reliable control of a nuclear ramjet, it is necessary to provide materials and components for the control system which will operate in an environment dictated by the nuclear characteristics of the system. A similar problem is encountered in providing nuclear propulsion for manned aircraft. Much work has been done on establishing reliable components for this purpose; however, the environment to be encountered in missile applications is more severe. Thus, it was necessary to accumulate as much available data as possible on radiation effects and then extend the data experimentally to cover the particular problems encountered with PLUTO.

Additional Information

On January 1, 1957, the U.S. Air Force and the U.S. Atomic Energy Commission selected the Lawrence Livermore National Laboratory’s (LLNL) predecessor, the Lawrence Radiation Laboratory, to study the feasibility of applying heat from nuclear reactors to ramjet engines. This research became known as “Project Pluto“. The work was directed by Dr. Ted Merkle, leader of the laboratory’s R-Division.

Originally carried out at Livermore, California, the work was moved to new facilities constructed for $1.2 million on 8 square miles (21 km2) of Jackass Flats at the NTS, known as Site 401. The complex consisted of 6 miles (10 km) of roads, critical assembly building, control building, assembly and shop buildings, and utilities. Also required for the construction was 25 miles (40 km) of oil well casing which was necessary to store the approximately 1,000,000 pounds (450,000 kg) of pressurized air used to simulate ramjet flight conditions for Pluto.

The principle behind the nuclear ramjet was relatively simple: motion of the vehicle pushed air in through the front of the vehicle (ram effect), a nuclear reactor heated the air, and then the hot air expanded at high speed out through a nozzle at the back, providing thrust.

The notion of using a nuclear reactor to heat the air was fundamentally new. Unlike commercial reactors, which are surrounded by concrete, the Pluto reactor had to be small and compact enough to fly, but durable enough to survive a 7,000-mile (11,000 km) trip to a potential target. The nuclear engine could, in principle, operate for months, so a Pluto cruise missile could be left airborne for a prolonged time before being directed to carry out its attack.

The success of this project would depend upon a series of technological advances in metallurgy and materials science. Pneumatic motors necessary to control the reactor in flight had to operate while red-hot and in the presence of intense radiation. The need to maintain supersonic speed at low altitude and in all kinds of weather meant the reactor, code named “Tory”, had to survive high temperatures and conditions that would melt the metals used in most jet and rocket engines. Ceramic fuel elements would have to be used; the contract to manufacture the 500,000 pencil-sized elements was given to the Coors Porcelain Company.

The proposed use for nuclear-powered ramjets would be to power a cruise missile, called SLAM, for Supersonic Low Altitude Missile. In order to reach ramjet speed, it would be launched from the ground by a cluster of conventional rocket boosters. Once it reached cruising altitude and was far away from populated areas, the nuclear reactor would be made critical. Since nuclear power gave it almost unlimited range, the missile could cruise in circles over the ocean until ordered “down to the deck” for its supersonic dash to targets in the Soviet Union. The SLAM as proposed would carry a payload of many nuclear weapons to be dropped on multiple targets, making the cruise missile into an unmanned bomber. After delivering all its warheads, the missile could then spend weeks flying over populated areas at low altitudes, causing tremendous ground damage with its shock wave. When it finally lost enough power to fly, and crash-landed, the engine would have a good chance of spewing deadly radiation for months to come.

On May 14, 1961, the world’s first nuclear ramjet engine, “Tory-IIA”, mounted on a railroad car, roared to life for a few seconds. Three years later, “Tory-IIC” was run for five minutes at full power. Despite these and other successful tests the Pentagon, sponsor of the “Pluto project”, had second thoughts. The weapon was considered “too provocative”, and it was believed that it would compel the Soviets to construct a similar device, against which there was no known defense. Intercontinental ballistic missile technology had proven to be more easily developed than previously thought, reducing the need for such highly capable cruise missiles. On July 1, 1964, seven years and six months after it was started, “Project Pluto” was canceled.

The above was provided by Wikipedia.


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Naval Criminal Investigative Service (NCIS) Documents on Unidentified Submerged Objects or USOs


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Background

According to the NAVY, the NCIS has the following mission:

The Naval Criminal Investigative Service (NCIS) is the federal law enforcement agency charged with conducting investigations of felony-level offenses affecting the Navy and Marine Corps – that is, crimes punishable by confinement for more than one year.

NCIS also performs investigations and operations aimed at identifying and neutralizing foreign intelligence, international terrorist, and cyber threats to the Department of the Navy.

In addition, it provides warning of threats and specialized defensive force protection support to U.S. naval forces around the world.

Recently, I requested a copy of all NCIS investigations, which involved USOs and other unidentified objects found in the water.

To my surprise, some documents came up.

They can be downloaded below:


Declassified Documents

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Naval Criminal Investigative Service (NCIS) Documents on Unidentified Submerged Objects or USOs
[54 Pages, 8.9MB]

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Naval Criminal Investigative Service (NCIS) Documents Forwarded to Naval Surface Force, U.S. Pacific Fleet
[11 Pages, 3.1MB] – Additional records were released in September of 2016, however, not quite the intention. Still interesting, and archived for reference.


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Avrocar

The VZ-9-AV Avrocar (official designation but often listed as VZ-9) was a Canadian VTOL aircraft developed by Avro Aircraft Ltd. as part of a secret U.S. military project carried out in the early years of the Cold War.

The Avrocar intended to exploit the Coandă effect to provide lift and thrust from a single “turborotor” blowing exhaust out the rim of the disk-shaped aircraft to provide anticipated VTOL-like performance. In the air, it would have resembled a flying saucer.

Two prototypes were built as “proof-of-concept” test vehicles for a more advanced USAF fighter and also for a U.S. Army tactical combat aircraft requirement. In flight testing, the Avrocar proved to have unresolved thrust and stability problems that limited it to a degraded, low-performance flight envelope; subsequently, the project was cancelled in 1961.



When flown without tethers, the Avrocar was unstable
and could reach top speed of only 35 mph.
(U.S. Air Force photo)


Declassified Documents


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The Avrocar Flight Test Plan, 15 July 1959
[14 Pages, 1mb]

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Analysis of Tests of the Avrocar in the NASA 40 x 80ft Wind Tunnel, Ames Research Center, February 1961
[298 Pages, 187MB] – An analysis is presented of some aspects of the full scale wind tunnel tests of the Avrocar vehicle. Methods used to analyze force and pressure data are formulated and results are compared with theory and small scale model tests. Aerodynamically, the performance demonstrated by the first Avrocar vehicle in its initial configuration was disappointing in that a low lift curve slop, a large nose-up pitching moment and insufficient jet vectoring capability precluded flight in free air and in the ground cushion above about 35 mph. Modifications to the aircraft based on these and other test results have been made, the major change being in the redesign of the trailing edge region where a rearwardfacing nozzle, containing a pitch control vane to provide adequate jet vectoring control, has been incorporated. The jet flap effect thus obtained is expected to allow flight in free-air as well as at higher speeds in the ground cushion.

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History of the Air Force Flight Test Center, Edwards Air Force Base, California, 1 January – 30 June 1961
[4 Pages, 1.69mb]This is a partial release of this document, which includes only the portion on the Avrocar and the title page.



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Bell Rocket Jet Pack (Individual Lift Device)

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In the early 1960s, Bell Aerosystems built a rocket pack which it called the “Bell Rocket Belt” or “man-rocket” for the US Army, using hydrogen peroxide as fuel. This concept was revived in the 1990s and today these packs can provide powerful, manageable thrust. This rocket belt’s propulsion works with superheated water vapor. A gas cylinder contains nitrogen gas, and two cylinders containing highly concentrated hydrogen peroxide. The nitrogen presses the hydrogen peroxide onto a catalyst, which decomposes the hydrogen peroxide into a mixture of superheated steam and oxygen with a temperature of about 740 °C. This was led by two insulated curved tubes to two nozzles where it blasted out, supplying the recoil. The pilot can vector the thrust by altering the direction of the nozzles through hand-operated controls. To protect from resulting burns the pilot had to wear insulating clothes.

One Bell Rocket Belt is on display at the Smithsonian Institution’s, National Air and Space Museum annex, the Steven F. Udvar-Hazy Center, located near Dulles Airport.


Available Documents

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Small Rocket Lift Device, November 1961 [ 186 Pages, 4.54MB ]

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Individual Lift Device Records from the U.S. Army, 15 October [URL='http://documents.theblackvault.com/documents/liftdevice.pdf']1967 [ 93 Pages, 4.54MB ][/URL]


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Insectothopter, CIA’s UAV from the 1970s

21 February, 2015

The Insectothopter was a miniature unmanned aerial vehicle developed by the United States Central Intelligence Agency’s research and development office in the 1970s. The Insectothopter was the size of a dragonfly, and was hand-painted to look like one. It was powered by a small gasoline engine to make the wings move and was fueled by a very small amount of gas. The project was abandoned when the Insectothopter was found to be too difficult to control in crosswinds.

The CIA produced and released the below video, and FOIA requests are currently being processed for additional documented information.


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Operation Mockingbird

Operation Mockingbird was a secret campaign by the United States Central Intelligence Agency (CIA) to influence media. Begun in the 1950s, it was initially organized by Cord Meyer and Allen W. Dulles, it was later led by Frank Wisner after Dulles became the head of the CIA. The organization recruited leading American journalists into a network to help present the CIA’s views, and funded some student and cultural organizations, and magazines as fronts. As it developed, it also worked to influence foreign media and political campaigns, in addition to activities by other operating units of the CIA.

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CIA Records on Operation Mockingbird [6 Pages, 1.46MB] – According to the CIA, these are all the records available on Mockingbird.

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Project Blue Book

Project Blue Book was one of a series of systematic studies of Unidentified flying objects (UFOs) conducted by the United States Air Force (U.S.A.F.). Started in 1952, it was the second revival of such a study. A termination order was given for the study in December 1969, and all activity under its auspices ceased in January 1970.



Air Force History’s Referencing UFOs in the Blue Book Era

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History of the Directorate of Intelligence June 1 – December 31 1952
[13 Pages, 3MB]

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History of the 5th Air Force, Daily Intel Summary, October 1952 [7 Pages, 1.7MB]

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History of the 5th Air Force, Daily Intel Summary, August 1952
[7 Pages, 1.5MB]

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Lessons Learned, Headquarters, 52d Combat Aviation Battalion, 22 September 1969 [54 Pages, 3MB] – It is unclear if this document is part of the Blue Book system. It does confirm, however, that towards the end of the Blue Book era, military installations were still seeing UFOs – some they were later able to identify – while others they were not.


The Condon Committee Report

The report contains the results of a scientific inquiry into the phenomena of Unidentified Flying Objects.

This volume contains: (1) The scientific context, (2) Appendices A-X, and (3) The index.

These are searchable .pdf files, however, are quite large. Please note the file sizes.

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The Condon Report, Volume 1, January 1969 [529 Pages, 174MB]

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Documents in this Collection
Documents in PDF format require the Adobe Acrobat Reader®


(EST PUB DATE) INVISIBLE PHOTOGRAPHY AND WRITING, SYMPATHETIC INK, ETC.
Document Number: CIA-RDP11X00001R000100010003-7

Pages: 2
Attachment
Size : 220.04 KB
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CIA-RDP11X00001R000100010003-7.pdf 220.04 KB


(EST PUB DATE) SECRET WRITING
Document Number: CIA-RDP11X00001R000100010002-8
Pages: 1
Attachment
Size : 47.18 KB
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CIA-RDP11X00001R000100010002-8.pdf 47.18 KB


GERMAN SECRET INK. FORMULAS USED IN PREPARATION OF. SOURCE-N.G.
Document Number: CIA-RDP11X00001R000100010006-4
Pages: 3
Attachment
Size 104.52 KB
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CIA-RDP11X00001R000100010006-4.pdf 104.52 KB


MEMORANDUM TO FRANK V. MARTENEK FROM AMHEINZELMANN RE SAMPLES MOST SUITED ON YOUR LIST
Document Number: CIA-RDP11X00001R000100010004-6
Pages: 1
Attachment
Size 45.84 KB
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CIA-RDP11X00001R000100010004-6.pdf 45.84 KB


MISC RE HOW TO OPEN SEALED LETTERS
Document Number: CIA-RDP11X00001R000100010001-9
Pages: 6
Attachment
Size
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CIA-RDP11X00001R000100010001-9.pdf 377.7 KB


GERMAN SECRET INK. FORMULAS USED IN PREPERATION OF. SOURCE - N.G.
Document Number: CIA-RDP11X00001R000100010005-5
Pages: 1
Attachment
Size 45.88 KB
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CIA-RDP11X00001R000100010005-5.pdf 45.88 KB

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In November, the CIA announced it would publish the material, and the entire declassified CREST archive is now available on the CIA Library website.

- THE BERLIN TUNNEL OPERATION 1952-1956

Document Number: CIA-RDP07X00001R000100010001-9
Pages: 100
Attachment Size 4.11 MB
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CIA-RDP07X00001R000100010001-9.pdf 4.11 MB


 

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