Whitecaps

Commentary and information about public safety and security, intelligence and counterintelligence, open government and secrecy, and other issues in northern Idaho and eastern Washington.

Name:
Location: Coeur d'Alene, Idaho, United States

Raised in Palouse, WA. Graduated from Washington State University. US Army (Counterintelligence). US Secret Service (Technical Security Division) in Fantasyland-on-the-Potomac and Los Angeles. Now living in north Idaho.


Wednesday, February 23, 2005

It's (Probably) Not a Flying Saucer

If in the near future you happen to be up along the Canadian border and see what appears to be an unidentified flying object...smile. You may be on candid camera...mounted on a US government unmanned aerial vehicle (UAV).

It has evidently finally dawned on some of our legislators that the technology being used to gather data and images in Iraq and Iran (remember their flying saucer scare several weeks ago) might be able to help protect our own borders. (That revelation qualifies for a "Duh!")

On February 7, 2005, The Library of Congress, Congressional Research Service, released a six-page report for Congress entitled Homeland Security: Unmanned Aerial Vehicles and Border Security. This report examines the strengths and weaknesses of deploying UAVs along our borders, particularly in areas especially difficult for human agents to monitor. It also discusses the issues Congress will have to consider in making the decision to deploy or not.

Though civil liberties are a big concern whenever spy technology is deployed, the use of UAVs has a lot of potential in non-law enforcement areas. For example, it seems to me that a UAV equipped with appropriate sensors could fly over a major forest fire at lower altitudes in conditions of more limited visibility to gather and send back critical data about the fire. If a UAV can operate in more hostile environments to gather and transmit more timely data safer than a manned aircraft, it seems like a worthwhile investment.

1 Comments:

Blogger retrodynamic said...

Technology Submission - Novel Rotary-Turbo-InFlow Tech - Featured Development

GEARTURBINE PROJECT
Atypical InFlow Thermodynamic
Technology Proposal Submission
Novel Fueled Motor Engine Type

*State of the art Innovative concept Top system Higher efficient percent.
Have similar system of the Aeolipile Heron Steam device from Alexandria 10-70 AD.

http://www.youtube.com/watch?v=0cPo9Lf44TE

YouTube; * Atypical New • GEARTURBINE / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type - Non Waste Looses

*8-X/Y Thermodynamic CYCLE - Way Steps:
1)1-Compression / bigger
2)2-Turbo 1 cold
3)2-Turbo 2 cold
4)2-Combustion - circular motion flames / opposites
5)2-Thrust - single turbo & planetary gears / ying yang
6)2-Turbo 2 hot
7)2-Turbo 1 hot
8)1-Turbine / bigger

-New Form-Function Motor-Engine Device. Next Step, Epic Design Change, Broken-Seal Revelation. -Desirable Power-Plant Innovation.

-With Retrodynamic Dextrogiro vs. Levogiro Phenomenon Effect. / Rotor-RPM VS InFlow / front to front; "Collision-Interaction Type" - inflow vs. blades-gear-move. Technical unique dynamic innovative motion mode. [Retrodynamic Reaction = When the inflow have more velocity the rotor have more RPM Acceleration, with high (XY Position) Momentum] Which the internal flow (and rotor) duplicate its speed, when activated being in a rotor (and inflow) with [inverse] opposite Turns. A very strong Novel concept of torque power thrust.

-Non-waste parasitic looses system for cooling, lubrication & combustion.

-Shape-Mass + Rotary-Motion = Inertia-Dynamic / Form-Function Wide [Flat] Cylindrical shape + positive dynamic rotary mass = continue Inertia kinetic positive tendency motion. Like a Flywheel.

-Combustion 2Two continue circular [Rockets] flames. [ying yang] opposite to the other. – With 2TWO very long distance INFLOW [inside propulsion] CONDUITS. -4 TURBOS Rotary Total Thrust-Power Regeneration Power System. -Mechanical direct 2two [Small] Planetary Gears at polar position. -Like the Ying Yang Symbol/Concept. -Wide out the Rotor circumference were have much more lever [HIGH Torque] POWER THRUST. -Military benefits; No blade erosion by sand & very low heat target signature profile. -3 points of power thrust; 1-flow way, 2-gear, 3-turbine. *Patent; Dic. 1991 IMPI Mexico #197187 All Rights Reserved. Carlos Barrera.

1:13 PM, August 17, 2013  

Post a Comment

<< Home