Tailer's Family - journeying!
Project - RAF Waddington Air Show
CHIPMUNK T.10 (G-BYHL) WG308 8
belonging to M R & I D Higgins.
with KC-135 STRATOTANKER behind it.
----------------------------------------------------------------------------------------------
Four DHC-1Chipmunks commenced service with the Aircraft Squadron in 1957. They were replacements for the Tiger Moths and <Harvards which were being phased out. These Chipmunks, also affectionately known as "Chippies", served the Force until 1960, the year that saw the disbandment of MAAF (Singapore Wing)..
The Chipmunk was designed in Canada by Wsiewolod J. Jakimuik, previously Chief Designer for PZL in Poland. It was developed by de Havilland Aircraft of Canada as a military training aircraft to replace the legendry DH.82 Tiger Moth.
This trainer, is a low wing monoplane of all metal, stressed skin construction with the pilot and instructor seated in tandem under a single piece sliding canopy.
The prototype first flew on 22 May 1946 from de Havilland's factory at Downsview, Toronto. Although designed in Canada, the Chipmunk was built in large numbers in Great Britain for the RAF. The British products carried the mark number T.10.
The Chipmunk T.10 serves with the RAF and differs from the Canadian T.1 in that the T.10 was fully aerobatic from the outset. The T.10 also featured a multi-panel sliding canopy whilst most Canadian-built Chipmunks had a bubble canopy.
Specifications
Manufacturer : De Havilland Aircraft of Canada.
Crew : Two in tandem, pilot and trainee.
Length: 7.75 m
Height: 2.13 m
Wing span: 10.46 m
Wing area : 15.97 m2
Performance
Speed: 222 km/h at sea level
Range : 451km
Climb : 256m/min
Weight: (empty): 646 kg
Max.Take-off Weight: 914 kg
Service ceiling : 5,200 m
Propulsion
Powerplant: 1 x 108kw (145 hp) Gipsy Major 8,
-cylinder incline air-cooled.
T.10 served with the Royal Air Force.
Malayan Auxiliary Air Force Singapore Wing
KC-135 STRATOTANKER
KC-135 Stratotanker
• KC-135 Stratotanker
Related Stories
• Upgraded KC-135 Stratotankers integral to joint force - 9/21/2006
• KC-135 launch - 9/19/2006
• Maintainers improving system through AFSO 21 - 9/18/2006
• KC-135's 50 years of service recognized - 9/14/2006
• Airman celebrates different KC-135 anniversary - 9/13/2006
• Airman celebrates different KC-135 anniversary - 9/12/2006
• Civic leaders, media help celebrate KC-135's 50th anniversary - 9/11/2006
• Former KC-135 pilot reminisces about plane's glory days - 9/6/2006
• Retired chief can't say goodbye to KC-135 - 9/6/2006
• KC-135s take on aeromedical evacuation role - 8/9/2006
Mission
The KC-135 Stratotanker's principal mission is air refueling. This unique asset greatly enhances the Air Force's capability to accomplish its primary missions of Global Reach and Global Power. It also provides aerial refueling support to Air Force, Navy and Marine Corps aircraft as well as aircraft of allied nations. The KC-135 is also capable of transporting litter and ambulatory patients using patient support pallets during aeromedical evacuations.
Features
Four turbofans, mounted under 35-degree swept wings, power the KC-135 to takeoffs at gross weights up to 322,500 pounds (146,285 kilograms). Nearly all internal fuel can be pumped through the flying boom, the KC-135's primary fuel transfer method. A special shuttlecock-shaped drogue, attached to and trailing behind the flying boom, may be used to refuel aircraft fitted with probes. Some aircraft have been configured with the Multipoint Refueling System or MPRS. MPRS configured aircraft are capable of refueling two receiver aircraft simultaneously from special “pods” mounted on the wingtips. One crewmember, known as the boom operator, is stationed in the rear of the plane and controls the boom during in-flight air refueling. A cargo deck above the refueling system can hold a mixed load of passengers and cargo. Depending on fuel storage configuration, the KC-135 can carry up to 83,000 pounds (37,648 kilograms) of cargo.
Background
Air Mobility Command manages more than 490 total aircraft inventory Stratotankers, of which the Air Force Reserve and Air National Guard fly 271 of those in support of AMC's mission.
The Boeing Company's model 367-80 was the basic design for the commercial 707 passenger plane as well as the KC-135A Stratotanker. In 1954 the Air Force purchased the first 29 of its future 732-plane fleet. The first aircraft flew in August 1956 and the initial production Stratotanker was delivered to Castle Air Force Base, Calif., in June 1957. The last KC-135 was delivered to the Air Force in 1965.
Of the original KC-135A's, more than 410 have been modified with new CFM-56 engines produced by CFM-International. The re-engined tanker, designated either the KC-135R or KC-135T, can offload 50 percent more fuel, is 25 percent more fuel efficient, costs 25 percent less to operate and is 96 percent quieter than the KC-135A.
Under another modification program, 157 Air Force Reserve and Air National Guard tankers were re-engined with the TF-33-PW-102 engines. The re-engined tanker, designated the KC-135E, is 14 percent more fuel efficient than the KC-135A and can offload 20 percent more fuel.
Through the years, the KC-135 has been altered to do other jobs ranging from flying command post missions to reconnaissance. RC-135s are used for special reconnaissance and Air Force Materiel Command's NKC-135A's are flown in test programs. Air Combat Command operates the OC-135 as an observation platform in compliance with the Open Skies Treaty.
Over the next few years, the aircraft will undergo upgrades to expand its capabilities and improve its reliability. Among these are improved communications, navigation and surveillance equipment to meet future civil air traffic control needs.
General Characteristics
Primary Function: Aerial refueling and airlift
Prime Contractor: The Boeing Company
Power Plant: KC-135R/T, CFM International CFM-56 turbofan engines; KC-135E, Pratt and Whitney TF-33-PW-102 turbofan engines
Thrust: KC-135R, 21,634 pounds each engine; KC-135E, 18,000 pounds each engine
Wingspan: 130 feet, 10 inches (39.88 meters)
Length: 136 feet, 3 inches (41.53 meters)
Height: 41 feet, 8 inches (12.7 meters)
Speed: 530 miles per hour at 30,000 feet (9,144 meters)
Ceiling: 50,000 feet (15,240 meters)
Range: 1,500 miles (2,419 kilometers) with 150,000 pounds (68,039 kilograms) of transfer fuel; ferry mission, up to 11,015 miles (17,766 kilometers)
Maximum Takeoff Weight: 322,500 pounds (146,285 kilograms)
Maximum Transfer Fuel Load: 200,000 pounds (90,719 kilograms)
Maximum Cargo Capability: 83,000 pounds (37,648 kilograms), 37 passengers
Pallet Positions: 6
Crew: Three: pilot, co-pilot and boom operator. Some KC-135 missions require the addition of a navigator. The Air Force has a limited number of navigator suites that can be installed for unique missions.
Aeromedical Evacuation Crew: A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions. Medical crew may be altered as required by the needs of patients.
Unit Cost: $39.6 million (FY98 constant dollars)
Date Deployed: August 1956
Inventory: Active duty, 195; Air National Guard, 251; Air Force Reserve, 84
Point of Contact
Air Mobility Command, Public Affairs Office; 503 Ward Drive Ste 214, Scott AFB, IL 62225-5335, DSN 779-7843 or 618-229-7843.
July 2006
KC-135 Stratotanker
Air Force Link
Project - RAF Waddington Air Show
CHIPMUNK T.10 (G-BYHL) WG308 8
belonging to M R & I D Higgins.
with KC-135 STRATOTANKER behind it.
----------------------------------------------------------------------------------------------
Four DHC-1Chipmunks commenced service with the Aircraft Squadron in 1957. They were replacements for the Tiger Moths and <Harvards which were being phased out. These Chipmunks, also affectionately known as "Chippies", served the Force until 1960, the year that saw the disbandment of MAAF (Singapore Wing)..
The Chipmunk was designed in Canada by Wsiewolod J. Jakimuik, previously Chief Designer for PZL in Poland. It was developed by de Havilland Aircraft of Canada as a military training aircraft to replace the legendry DH.82 Tiger Moth.
This trainer, is a low wing monoplane of all metal, stressed skin construction with the pilot and instructor seated in tandem under a single piece sliding canopy.
The prototype first flew on 22 May 1946 from de Havilland's factory at Downsview, Toronto. Although designed in Canada, the Chipmunk was built in large numbers in Great Britain for the RAF. The British products carried the mark number T.10.
The Chipmunk T.10 serves with the RAF and differs from the Canadian T.1 in that the T.10 was fully aerobatic from the outset. The T.10 also featured a multi-panel sliding canopy whilst most Canadian-built Chipmunks had a bubble canopy.
Specifications
Manufacturer : De Havilland Aircraft of Canada.
Crew : Two in tandem, pilot and trainee.
Length: 7.75 m
Height: 2.13 m
Wing span: 10.46 m
Wing area : 15.97 m2
Performance
Speed: 222 km/h at sea level
Range : 451km
Climb : 256m/min
Weight: (empty): 646 kg
Max.Take-off Weight: 914 kg
Service ceiling : 5,200 m
Propulsion
Powerplant: 1 x 108kw (145 hp) Gipsy Major 8,
-cylinder incline air-cooled.
T.10 served with the Royal Air Force.
Malayan Auxiliary Air Force Singapore Wing
KC-135 STRATOTANKER
KC-135 Stratotanker
• KC-135 Stratotanker
Related Stories
• Upgraded KC-135 Stratotankers integral to joint force - 9/21/2006
• KC-135 launch - 9/19/2006
• Maintainers improving system through AFSO 21 - 9/18/2006
• KC-135's 50 years of service recognized - 9/14/2006
• Airman celebrates different KC-135 anniversary - 9/13/2006
• Airman celebrates different KC-135 anniversary - 9/12/2006
• Civic leaders, media help celebrate KC-135's 50th anniversary - 9/11/2006
• Former KC-135 pilot reminisces about plane's glory days - 9/6/2006
• Retired chief can't say goodbye to KC-135 - 9/6/2006
• KC-135s take on aeromedical evacuation role - 8/9/2006
Mission
The KC-135 Stratotanker's principal mission is air refueling. This unique asset greatly enhances the Air Force's capability to accomplish its primary missions of Global Reach and Global Power. It also provides aerial refueling support to Air Force, Navy and Marine Corps aircraft as well as aircraft of allied nations. The KC-135 is also capable of transporting litter and ambulatory patients using patient support pallets during aeromedical evacuations.
Features
Four turbofans, mounted under 35-degree swept wings, power the KC-135 to takeoffs at gross weights up to 322,500 pounds (146,285 kilograms). Nearly all internal fuel can be pumped through the flying boom, the KC-135's primary fuel transfer method. A special shuttlecock-shaped drogue, attached to and trailing behind the flying boom, may be used to refuel aircraft fitted with probes. Some aircraft have been configured with the Multipoint Refueling System or MPRS. MPRS configured aircraft are capable of refueling two receiver aircraft simultaneously from special “pods” mounted on the wingtips. One crewmember, known as the boom operator, is stationed in the rear of the plane and controls the boom during in-flight air refueling. A cargo deck above the refueling system can hold a mixed load of passengers and cargo. Depending on fuel storage configuration, the KC-135 can carry up to 83,000 pounds (37,648 kilograms) of cargo.
Background
Air Mobility Command manages more than 490 total aircraft inventory Stratotankers, of which the Air Force Reserve and Air National Guard fly 271 of those in support of AMC's mission.
The Boeing Company's model 367-80 was the basic design for the commercial 707 passenger plane as well as the KC-135A Stratotanker. In 1954 the Air Force purchased the first 29 of its future 732-plane fleet. The first aircraft flew in August 1956 and the initial production Stratotanker was delivered to Castle Air Force Base, Calif., in June 1957. The last KC-135 was delivered to the Air Force in 1965.
Of the original KC-135A's, more than 410 have been modified with new CFM-56 engines produced by CFM-International. The re-engined tanker, designated either the KC-135R or KC-135T, can offload 50 percent more fuel, is 25 percent more fuel efficient, costs 25 percent less to operate and is 96 percent quieter than the KC-135A.
Under another modification program, 157 Air Force Reserve and Air National Guard tankers were re-engined with the TF-33-PW-102 engines. The re-engined tanker, designated the KC-135E, is 14 percent more fuel efficient than the KC-135A and can offload 20 percent more fuel.
Through the years, the KC-135 has been altered to do other jobs ranging from flying command post missions to reconnaissance. RC-135s are used for special reconnaissance and Air Force Materiel Command's NKC-135A's are flown in test programs. Air Combat Command operates the OC-135 as an observation platform in compliance with the Open Skies Treaty.
Over the next few years, the aircraft will undergo upgrades to expand its capabilities and improve its reliability. Among these are improved communications, navigation and surveillance equipment to meet future civil air traffic control needs.
General Characteristics
Primary Function: Aerial refueling and airlift
Prime Contractor: The Boeing Company
Power Plant: KC-135R/T, CFM International CFM-56 turbofan engines; KC-135E, Pratt and Whitney TF-33-PW-102 turbofan engines
Thrust: KC-135R, 21,634 pounds each engine; KC-135E, 18,000 pounds each engine
Wingspan: 130 feet, 10 inches (39.88 meters)
Length: 136 feet, 3 inches (41.53 meters)
Height: 41 feet, 8 inches (12.7 meters)
Speed: 530 miles per hour at 30,000 feet (9,144 meters)
Ceiling: 50,000 feet (15,240 meters)
Range: 1,500 miles (2,419 kilometers) with 150,000 pounds (68,039 kilograms) of transfer fuel; ferry mission, up to 11,015 miles (17,766 kilometers)
Maximum Takeoff Weight: 322,500 pounds (146,285 kilograms)
Maximum Transfer Fuel Load: 200,000 pounds (90,719 kilograms)
Maximum Cargo Capability: 83,000 pounds (37,648 kilograms), 37 passengers
Pallet Positions: 6
Crew: Three: pilot, co-pilot and boom operator. Some KC-135 missions require the addition of a navigator. The Air Force has a limited number of navigator suites that can be installed for unique missions.
Aeromedical Evacuation Crew: A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions. Medical crew may be altered as required by the needs of patients.
Unit Cost: $39.6 million (FY98 constant dollars)
Date Deployed: August 1956
Inventory: Active duty, 195; Air National Guard, 251; Air Force Reserve, 84
Point of Contact
Air Mobility Command, Public Affairs Office; 503 Ward Drive Ste 214, Scott AFB, IL 62225-5335, DSN 779-7843 or 618-229-7843.
July 2006
KC-135 Stratotanker
Air Force Link