Posted on 08/11/2003 2:37:31 AM PDT by snippy_about_it
101st on Patrol
![]() Private 1st Class Samuel Wright, 20, of C Co., 326th Engineering Battalion of the 101st Airborne Division, carries a picture of Saddam Hussein found during a patrol Wednesday, July 30, 2003, in Sinjar, Iraq. ( AP Photo /Sergei Grits ) ![]() US troops with the 187th Infantry Regiment, 101st Airborne Division, begin to patrol al Alrisala, 50 miles (80 kms) south of Mosul on Saturday, Aug. 2, 2003. ( AP Photo /Sergei Grits ) ![]() A U.S soldier with the 187th Infantry Regiment, 101st Airborne Division, patrols al Alrisala, 50 miles (80 kms) south of Mosul on Saturday, Aug. 2, 2003. (AP Photo /Sergei Grits) ![]() U.S. soldiers patrol near the area where Sergeant Leonard Simmons from Charlie Company, 3rd Battalion, 502nd infantry Regiment, 101st Airborne Div., memorial service will be taking place, in Mosul, Sunday Aug.10, 2003.Simmons, who was from Clarksville, Tennessee, died of cardiac arrest on Aug.6, 2003, while on duty. (AP Photo/Manish Swarup) ![]() U.S. soldiers from the 101st Airborne Division play chess before leaving for a patrol, at an army base near Mosul, Iraq, Friday Aug. 8, 2003. (AP Photo/Manish Swarup) ![]() US Army Spc. Shane Boyd, of Chattanooga, Tenn., First Battalion, 187th Infantry Regiment, 101st Airborne Division, reads a book during a break in his service in headquaters of his unit in an abandoned Iraqi army facility near of the town of Tall Afar, northern Iraq, Monday, Aug 4, 2002. (AP Photo/Sergei Grits )
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General Characteristics
Class: LCAC 1
Builder: Textron Marine and Land Systems/Avondale Gulfport Marine
Power Plant: 4- Avco-Lycoming TF-40B gas turbines (2 for propulsion/2 for lift); 16,000 hp sustained; 2- shrouded reversible pitch airscrews; 4- double-entry fans, centrifugal or mixed flow (lift)
Length: 87 feet 11 inches (26.4 meters)
Beam: 47 feet (14.3 meters)
Displacement: 87.2 tons (88.60 metric tons) light; 170-182 tons (172.73 - 184.92 metric tons) full load
Range: 200 miles at 40 kts with payload / 300 miles at 35 kts with payload
Speed: 40+ knots (46+ mph; 73.6 kph) with full load
Load Capacity: 60 tons / 75 ton overload
Military lift: 24 troops or 1 MBT
Crew: Five
Armament: 2 - 12.7mm MGs. Gun mounts will support: M-2HB .50 cal machine gun; Mk-19 Mod3 40mm grenade launcher; M-60 machine gun
Radars: Navigation: Marconi LN 66; I band
Date Deployed: 1982
Air Power |
The Convair B-58 Hustler was the first United States bomber to have a supersonic dash capability and required the development of much new technology. Although the B-58 was thought by many to be the harbinger of future generations of more advanced supersonic bombers, only about 115 of these unique aircraft were built, and they were quietly withdrawn from the SAC inventory after less than 10 years of service.
The general operating requirement, SAB-51, called for the replacement of the B-47 to be the first supersonic bomber. Research and development studies began in the late 1940's, and both Boeing and Convair developed conceptual designs. In 1952, the more revolutionary Convair design was chosen and designated the B-58, with the first flight occurring November 11, 1956. The program was not a competitive development, and Convair was given total development responsibility. As a result of money and schedule problems, the number of aircraft produced was reduced from 244 to 116, with its initial deployment in 1960.
The first B-58 was delivered in August 1960 and by 1964 deployment had reached about 90 aircraft. The B-58 had a Mach 2 dash capability and employed an external weapons pod. The last B-58 was retired in January 1970, about three months after the first FB-111 was accepted by SAC. Although the aircrews swore by the B-58, money and mission limitations led to it being phased out of the inventory after only 10 years of service.
The B-58 represented a drastic change from the B-47 in design, acquisition strategy, and deployment philosophy with SAB-51 being the first time that Air Force requirements called for radical, technological advances. The design specifications called for a Mach 2, high-altitude, medium-range nuclear bomber of minimum size to keep a low RCS. Convair was the prime contractor under the "Weapon System Management Concept" introduced with the B-58 and had responsibility for all subcontractor performance. This was in marked contrast to prior programs in which the Air Force was responsible for providing the prime contractor with "off-the-shelf" technology subsystems. The deployment concept was also different from the B-47 since the B-58 was designed to rely on quality rather than quantity.
These radical changes in the Air Force's approach to bomber development resulted in many problems. For example, meeting the technological requirements proved difficult and resulted in schedule slippages and cost overruns, while under-funding and lack of space on board affected development options. Subsequently, the B-58 was considered an interim bomber since the XB-70 was on the drawing boards.
The high altitude range of 3,500 nm for the B-58A and 4,000 nm for the B-58B included the use of a large centerline fuel pod. Although this range was better than the B-47, the lack of forward basing resulted in a requirement for more tanker support. While the B-58 was faster than Soviet fighters, the newly emerging threat was the development of SAMs in the late 1950's that forced the B-58 to adapt to low level penetration of enemy defenses. This change in mission profile caused a large increase in fuel consumption and compounded range problem.
The B-58, although the holder of numerous world speed records, was severely restricted in its usefulness and lifetime. Designed for supersonic, high-altitude penetration, the B-58 was limited in range, payload, and growth potential for the addition of advanced radar and other electronic equipment.
Thus, replacements were the main mode of modification. For example, analog electronic equipment with cooling problems was replaced by digital electronics. The B-58's planned production run was reduced because of the high cost per unit, a small payload, a mission profile different from its design concept, and, in the 1960's, a Secretary of Defense that downplayed the role of the bomber. In addition, it was very expensive to operate, and huge sums of money were needed for the Vietnam war.
Mission requirements for the Convair B-58 Hustler called for a subsonic cruise segment of several thousand miles followed by a supersonic dash (Mach 2.0) in the target zone of as much as 500 miles and, finally, a post-strike cruise segment. Diverse requirements such as these call for an aircraft of high aerodynamic efficiency at both subsonic and supersonic speeds, together with a versatile propulsion system capable of efficiently providing the required thrust in the different flight regimes. Today's response to the B-58 mission requirements would no doubt be a variable-sweep configuration employing afterburning turbofan engines. Unfortunately, the technology for a practical variable-sweep aircraft did not exist in the early 1950's when the B-58 was being designed - nor did afterburning turbofan engines. The only possible way in which the difficult mission objectives could be met in that time period was with the use of in-flight refueling.
With the increased effectiveness of enemy detection and antiaircraft capability discussed previously, the high-altitude Mach 2 method of weapons delivery became increasingly less viable, and an on-the deck method of attack became the preferred mode of operation. For this type of weapons delivery, however, the payload-range characteristics of the B-58 were much inferior to those of the B-52. For whatever reason, the last B-58 was withdrawn from service in January 1970 after about 10 years in the active inventory. First flight of the aircraft took place on November 11, 1956; approximately 115 units were built.
The B-58 represented a significant technical achievement in the 1950's time period, but the mission requirements called for innovations that far exceeded the technical state of the art then available.
Specifications:
Primary Function: Bomber
Contractor: Convair
Engines: Four General Electric J79-GE-1 turbojets of 15,000 lbs. thrust ea. with afterburner
Crew: Three - Pilot, Navigator/Bombardier, Defensive Systems Operator
Dimensions:
Span: 56 ft. 10 in.
Length: 96 ft. 10 in.
Height: 31 ft. 5 in.
Weights: Empty: 55,560 lb (25,201 kg) / Maximum Takeoff: 163,000 lb (73,935 kg)
Performance :
Maximum speed: 1,325 mph
Cruising speed: 610 mph.
Range: 4,400 miles max. ferry range
Service Ceiling: 64,800 ft.
Armaments:
one 20mm cannon in tail;
Up to 10,000-lb. bomb load of Nuclear or conventional weapons in pod or on under-wing pylons
For one pilot's life experiences with this airplane, please click here: Capt B.F. Brown's B-58 Page
All photos and information is Copyright of their owners
Thank goodness. lol. A cold shower or grapefruit juice in the eye, try those to wake up before getting so bad you need Darksheare's coffee. lol.
Yep, HMS Sheffield was hit by a french Exocet missle, fired from french Super-Etenard fighter-bombers, she shouldn't have taken as much damage as she did, the aluminum construction was part of the problem.
21 sailors lost their lives and a further 24 wounded.
The ship had to be abandoned eight hours after the flames had raged out of control. The ship's burnt out hulk sank a few days later on May 10th, whilst under the tow of frigate HMS Yarmouth. Position 53°04'S, 56°56' W. The first Royal Navy ship to be sunk in action for nearly forty years, the wreck is a designated war grave.
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