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The U.S. government has never successfully prosecuted anyone other than a government employee for disseminating unlawfully leaked classified information, Stone said in his testimony. Thus, the Supreme Court has never ruled on the constitutionality of such a prosecution.
Why doesn't Zaphod call his local FBI office and seek clarification? Tell them what you know. See what they have to say. You seem very confident in your position. Give them a call.
originally posted by: tsurfer2000h
a reply to: SlightlyAbovePar
Why doesn't Zaphod call his local FBI office and seek clarification? Tell them what you know. See what they have to say. You seem very confident in your position. Give them a call.
And what makes you think the FBI has any more valid info, and wouldn't that be the DOD that should be called?
originally posted by: MystikMushroom
originally posted by: tsurfer2000h
a reply to: SlightlyAbovePar
Why doesn't Zaphod call his local FBI office and seek clarification? Tell them what you know. See what they have to say. You seem very confident in your position. Give them a call.
And what makes you think the FBI has any more valid info, and wouldn't that be the DOD that should be called?
I was thinking the same thing. The FBI wouldn't know anything, heck -- most of the Airforce or other branches wouldn't either. There is a reason it's called a "Black" project. Highly compartmentalized.
The FBI would think Zaph is some nutjob, nothing more or less. There are a lot of mentally ill people that run around claiming to know state secrets -- I've ran into a few on the public transit system and standing on street corners.
This guy is just fear mongering and trying to discredit Zaph. Let's get back on topic everyone! Let's brainstorm and use our imaginations on what this could be!
Configuration Description
The vehicle type is stipulated as a low observable configuration for both the medium and high agility performance conditions, Sizing iterations resulted in a decision to represent both vehicle types in one configuration arrangement with the only principal differences being engine thrust level and mission fuel required.
This vehicle, Model 988-122/-123, is a single-place, subsonic all flying wing design powered by twin low bypass engines of 13,865 pounds dry thrust each. Externally, the vehicle, shown in general arrangement drawing ASC988-122-1, is characterized by the moderately swept leading edge at 48.75 degrees, lower surface inlet apertures, full span trailing edge elevons, and upper surface thrust vectoring exhaust nozzles. The wing leading edge incorporates large powered slats that are used to achieve critical maneuver conditions.
Control effectors include the yaw thrust vectoring exhaust nozzles with +45 degrees of deflection, upper and low Yaw Vane pairs integrated with the nozzle and lower surface, and four elevons per semi-span. Elevons are single panel at the most outboard and inboard position, with the two mid-span panels being split on the wing reference plane.
The interior layout, shown on inboard profile drawing ASC 988-122-2, provides sufficient room for all functional systems and features required. Principal features are the deep (approximately 15% t/c) center section for weapons bay, fuel tankage, crew station and equipment installations, include 30mm gun system installation. Basic thickness ratio decreases to approximately 8.5% at the main landing gear and then to 5% in the outboard panel.
The propulsion installation occupies a bay full chord length for each engine. The inlet is pitot type with a slightly offset diffuser duct.
Exhaust system features for the non-augmented engine consist of the fully offset duct turning through a circular bearing/rotation plane to direct exhaust gas through the rotating nozzle exit plane. The exhaust nozzle is a fixed throat SERN type that utilizes the inboard upper surface as an expansion surface.
Fuel tankage in the outer wing panel is integral. Center section fuel tankage above the weapons bay has main tank volume allocated as bladder protected "get-home" fuel.
originally posted by: TAGBOARD
From another online source, perhaps the Wichita sighting is of a variant of the Boeing Seattle concept, dating back to 1994 (CAGE Code 81208 - reference pages 114 to 129):
Boeing USAF Air Interdiction Model ASC 988-122/223
Configuration Description
The vehicle type is stipulated as a low observable configuration for both the medium and high agility performance conditions, Sizing iterations resulted in a decision to represent both vehicle types in one configuration arrangement with the only principal differences being engine thrust level and mission fuel required.
This vehicle, Model 988-122/-123, is a single-place, subsonic all flying wing design powered by twin low bypass engines of 13,865 pounds dry thrust each. Externally, the vehicle, shown in general arrangement drawing ASC988-122-1, is characterized by the moderately swept leading edge at 48.75 degrees, lower surface inlet apertures, full span trailing edge elevons, and upper surface thrust vectoring exhaust nozzles. The wing leading edge incorporates large powered slats that are used to achieve critical maneuver conditions.
Control effectors include the yaw thrust vectoring exhaust nozzles with +45 degrees of deflection, upper and low Yaw Vane pairs integrated with the nozzle and lower surface, and four elevons per semi-span. Elevons are single panel at the most outboard and inboard position, with the two mid-span panels being split on the wing reference plane.
The interior layout, shown on inboard profile drawing ASC 988-122-2, provides sufficient room for all functional systems and features required. Principal features are the deep (approximately 15% t/c) center section for weapons bay, fuel tankage, crew station and equipment installations, include 30mm gun system installation. Basic thickness ratio decreases to approximately 8.5% at the main landing gear and then to 5% in the outboard panel.
The propulsion installation occupies a bay full chord length for each engine. The inlet is pitot type with a slightly offset diffuser duct.
Exhaust system features for the non-augmented engine consist of the fully offset duct turning through a circular bearing/rotation plane to direct exhaust gas through the rotating nozzle exit plane. The exhaust nozzle is a fixed throat SERN type that utilizes the inboard upper surface as an expansion surface.
Fuel tankage in the outer wing panel is integral. Center section fuel tankage above the weapons bay has main tank volume allocated as bladder protected "get-home" fuel.