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The Harrier jump jet's primary distinguishing feature is its ability to operate exclusively from conventional, large airfields.
Answer: False
The Harrier jump jet is fundamentally distinguished by its capability for Vertical/Short Takeoff and Landing (V/STOL) operations, enabling it to operate from austere locations and aircraft carriers, rather than being restricted to conventional, large airfields.
The Harrier jump jet was initially developed by the American company McDonnell Douglas during the 1970s.
Answer: False
The Harrier jump jet was originally developed by the British manufacturer Hawker Siddeley in the 1960s, not by an American company in the 1970s.
The Harrier was the sole V/STOL aircraft design from the 1960s to achieve widespread practical success.
Answer: True
The Harrier's singular success underscores the considerable challenges in achieving practical V/STOL capabilities during the 1960s. It stood as the only demonstrably successful design amidst numerous contemporary attempts, validating its innovative engineering.
The Hawker Siddeley P.1154 served as the direct predecessor and development basis for the Harrier.
Answer: False
The Hawker Siddeley P.1127 is recognized as the direct predecessor to the Harrier, forming the foundational basis for its development, not the P.1154.
Hawker Aircraft initially designed its V/STOL concept to meet a NATO specification for a heavy bomber.
Answer: False
Hawker Aircraft's design efforts were initially directed towards fulfilling a NATO specification for a 'Light Tactical Support Fighter', not a heavy bomber.
The Hawker P.1154 project, intended for a NATO specification, was cancelled due to technical design flaws.
Answer: False
The Hawker P.1154 project was terminated by the incoming British government on February 2, 1965, primarily owing to concerns regarding its escalating costs during the prototype construction phase, not technical design flaws.
The Hawker Siddeley Kestrel was an operational variant utilized by the RAF for ground attack missions.
Answer: False
The Hawker Siddeley Kestrel served as an evaluation aircraft, utilized by a multinational 'Tri-partite Evaluation Squadron' to assess the operational viability of VTOL aircraft, rather than being an operational variant used by the RAF for ground attack.
The Hawker Siddeley P.1127 was a later variant of the Harrier, developed after the AV-8B.
Answer: False
The Hawker Siddeley P.1127 served as the direct predecessor and prototype aircraft for the Harrier, predating the AV-8B variant.
The 'Tri-partite Evaluation Squadron' utilized the Harrier GR.1 to test VTOL operational capabilities.
Answer: False
The 'Tri-partite Evaluation Squadron' conducted evaluations using the Hawker Siddeley Kestrel, a derivative of the P.1127, to assess VTOL operational capabilities, not the Harrier GR.1.
What is the primary capability that defines the Harrier jump jet?
Answer: Ability to operate from extremely short or vertical takeoffs and landings (V/STOL).
The Harrier jump jet is fundamentally distinguished by its capability for Vertical/Short Takeoff and Landing (V/STOL) operations, enabling it to operate from austere locations and aircraft carriers, rather than being restricted to conventional, large airfields.
Who was the original manufacturer of the Harrier jump jet, and in which decade was its development initiated?
Answer: Hawker Siddeley, 1960s
The Harrier jump jet originated from development by the British manufacturer Hawker Siddeley during the 1960s.
The Harrier's success in the 1960s is notable because it was:
Answer: The only truly successful V/STOL design among many attempts during that period.
The Harrier's singular success underscores the considerable challenges in achieving practical V/STOL capabilities during the 1960s. It stood as the only demonstrably successful design amidst numerous contemporary attempts, validating its innovative engineering.
Which aircraft served as the direct predecessor and development basis for the Harrier?
Answer: Hawker Siddeley P.1127
The Hawker Siddeley P.1127 is recognized as the direct predecessor to the Harrier, forming the foundational basis for its development.
What was the primary motivation behind the exploration of VTOL aircraft concepts in the 1950s?
Answer: To enable aircraft to operate without vulnerable, fixed runways.
The impetus for developing V/STOL aircraft in the 1950s stemmed from a strategic imperative to circumvent the vulnerability of fixed runways, thereby enabling aircraft operations independent of traditional airfield infrastructure.
What was the purpose of the Hawker Siddeley Kestrel?
Answer: To evaluate the operational capabilities of VTOL aircraft with a multinational squadron.
The Hawker Siddeley Kestrel served as an evaluation aircraft, utilized by a multinational 'Tri-partite Evaluation Squadron' to assess the operational viability of VTOL aircraft.
The cancellation of the Hawker P.1154 project was primarily due to:
Answer: Concerns over the project's cost.
The Hawker P.1154 project was terminated by the incoming British government on February 2, 1965, primarily owing to concerns regarding its escalating costs during the prototype construction phase.
The Hawker P.1154 was intended to meet a NATO specification for what type of aircraft?
Answer: Supersonic V/STOL Strike Fighter
The NATO NBMR-3 specification defined requirements for a supersonic V/STOL strike fighter. The Hawker P.1154 was designated to meet this specification.
The 'Tri-partite Evaluation Squadron' was formed to assess the operational use of which type of aircraft?
Answer: VTOL (Vertical Takeoff and Landing) aircraft
The 'Tri-partite Evaluation Squadron' conducted evaluations using the Hawker Siddeley Kestrel to assess the operational viability and methodologies for VTOL aircraft.
The acronym V/STOL denotes an aircraft's capability for Vertical/Short Takeoff and Landing.
Answer: True
V/STOL is an acronym denoting Vertical/Short Takeoff and Landing. This capability signifies the aircraft's capacity for vertical ascent or a significantly abbreviated ground roll, a defining characteristic differentiating it from conventional aircraft.
The Harrier's V/STOL capability was enabled by the innovative Pegasus engine, which utilized vectored thrust.
Answer: True
The pivotal engine technology enabling the Harrier's development, characterized by its vectored thrust capability, was designated the Pegasus.
The 'shipborne rolling vertical landing' (SRVL) technique allows the Harrier to land vertically without any forward speed.
Answer: False
Shipborne Rolling Vertical Landing (SRVL) is a specific landing methodology employed by the Harrier. It involves a near-vertical descent coupled with a degree of forward velocity, not landing vertically without any forward speed.
Wind direction is irrelevant for Harrier VTOL operations as long as the pilot maintains control.
Answer: False
Wind direction is a critical factor in Harrier V/STOL operations. Misalignment with the wind entering the engine intake can induce yawing moments, potentially resulting in control loss due to intake momentum drag. Pilots utilize wind vanes to ensure precise alignment.
During a vertical takeoff, the Harrier's nozzles are pointed directly downwards, and the pilot uses throttle adjustments for altitude control.
Answer: True
A vertical takeoff procedure for the Harrier involves positioning the aircraft into the wind, directing the swiveling engine nozzles vertically downwards, and advancing the throttle to maximum power. Pilot control of throttle adjustments is essential for maintaining a stable hover at the target altitude.
A short takeoff for the Harrier involves pointing the nozzles fully downwards during a conventional takeoff roll.
Answer: False
A short takeoff involves a conventional ground roll with the engine nozzles rotated partially downwards (less than 90 degrees) at a speed typically around 65 knots, not fully downwards.
The reaction control system utilizes bleed air directed through wingtip thrusters to aid control during hover.
Answer: True
The reaction control system (RCS) employs thrusters situated at the aircraft's extremities (nose, tail, and wingtips) to expel engine bleed air. This system is critical for providing directional control (pitch, roll, and yaw) during hover and low-speed flight regimes.
The 'Pegasus' engine was designed for high-subsonic speeds and relied on conventional jet thrust.
Answer: False
The Pegasus engine was central to the Harrier's V/STOL capability due to its vectored thrust system, which allowed directional control of engine exhaust for vertical lift or forward propulsion, not solely conventional jet thrust for high-subsonic speeds.
The 'intake momentum drag' phenomenon requires pilots to align the Harrier precisely with the wind during VTOL to prevent control loss.
Answer: True
The phenomenon of intake momentum drag arises when airflow entering the engine intake deviates from a perfectly axial path, generating a lateral force. This can precipitate a loss of directional control if not adequately mitigated, thereby rendering precise wind alignment imperative during VTOL maneuvers.
What does the acronym V/STOL stand for in the context of the Harrier aircraft?
Answer: Vertical/Short Takeoff and Landing
V/STOL is an acronym denoting Vertical/Short Takeoff and Landing. This capability signifies the aircraft's capacity for vertical ascent or a significantly abbreviated ground roll, a defining characteristic differentiating it from conventional aircraft.
The innovative engine technology central to the Harrier's V/STOL capability was known as the:
Answer: Pegasus Vectored Thrust
The Pegasus engine, developed by the Bristol Engine Company, was fundamental to the Harrier's V/STOL capability due to its integrated vectored thrust system.
What is the 'shipborne rolling vertical landing' (SRVL) technique?
Answer: A near-vertical landing with some forward speed to manage the undercarriage.
Shipborne Rolling Vertical Landing (SRVL) is a specific landing methodology employed by the Harrier. It involves a near-vertical descent coupled with a degree of forward velocity, a technique adopted to manage the structural limitations of the aircraft's outrigger undercarriage.
What is the significance of the 'intake momentum drag' issue mentioned in the source?
Answer: It requires precise wind alignment during VTOL to avoid control loss.
The phenomenon of intake momentum drag arises when airflow entering the engine intake deviates from a perfectly axial path, generating a lateral force. This can precipitate a loss of directional control if not adequately mitigated, thereby rendering precise wind alignment imperative during VTOL maneuvers.
The Harrier's ability to take off vertically requires the engine nozzles to be directed:
Answer: Vertically downwards.
A vertical takeoff procedure for the Harrier involves directing the swiveling engine nozzles vertically downwards.
Four main variants and three generations of the Harrier family were developed.
Answer: False
The Harrier family encompasses two primary generations and four principal variants, not three generations.
The Harrier GR.1 entered service with the Royal Air Force in 1969.
Answer: True
The Harrier GR.1 commenced official service with the Royal Air Force on April 18, 1969.
The United States Air Force, rather than the Marine Corps, was the first US military branch to procure the first-generation Harrier.
Answer: False
The United States Marine Corps (USMC) was the procuring entity for the first-generation Harrier, receiving AV-8A models, not the United States Air Force.
The British Aerospace Sea Harrier was a variant designed exclusively for land-based operations.
Answer: False
The British Aerospace Sea Harrier is a naval variant of the V/STOL jet, configured for fighter, reconnaissance, and attack roles, and was operated by the Royal Navy and the Indian Navy from aircraft carriers, not exclusively for land-based operations.
The informal name 'Shar' was commonly used for the Sea Harrier FRS.1 variant.
Answer: True
The Sea Harrier FRS.1 variant was colloquially referred to by the nickname 'Shar'.
The second-generation Harrier II (AV-8B/Harrier II) development involved collaboration between British Aerospace and Grumman.
Answer: False
The second-generation Harrier II development was a collaborative effort between British Aerospace and McDonnell Douglas, not Grumman.
The first production AV-8B Harrier II was delivered to the USMC in late 1983.
Answer: True
The initial production unit of the AV-8B Harrier II was delivered to the United States Marine Corps on December 12, 1983.
The RAF's first squadron equipped with the second-generation Harrier II became operational in the early 1990s.
Answer: True
The Royal Air Force operated the second-generation Harrier II, encompassing variants GR5, GR7, and GR9. The inaugural RAF squadron equipped with the Harrier II achieved operational status in December 1989, which falls within the early 1990s timeframe.
Harrier production ceased in the late 1990s, with over 1000 aircraft delivered.
Answer: False
Harrier production concluded in 2003, with a total of 824 aircraft delivered across all variants, not over 1000 in the late 1990s.
The Harrier GR9 and AV-8B+ Harrier had identical combat radii of 556 km.
Answer: True
The Harrier GR9 and the AV-8B+ Harrier variants shared an equivalent combat radius of 300 nautical miles (556 kilometers).
Only the second-generation Harrier variants, such as the AV-8B+, were equipped with radar systems.
Answer: False
While the AV-8B+ Harrier was equipped with radar, the Sea Harrier FA2 variant, which was also a second-generation aircraft, was equipped with radar systems as well. Therefore, it was not exclusively second-generation variants like the AV-8B+.
The Spanish Navy operated the AV-8S Matador, a variant of the Harrier jump jet.
Answer: True
The Spanish Navy operated the AV-8S Matador, a variant of the Harrier jump jet.
The 'Harrier II Plus' configuration refers to the final batch of remanufactured aircraft completed in 2003.
Answer: True
The 'Harrier II Plus' configuration denotes the final batch of remanufactured aircraft, with the last delivery occurring in December 2003, signifying the conclusion of the Harrier production line.
The Harrier GR.1 first entered service with which military branch and in what year?
Answer: Royal Air Force, 1969
The Harrier GR.1 commenced official service with the Royal Air Force on April 18, 1969.
Which US military branch was the initial operator of the first-generation Harrier (AV-8A)?
Answer: United States Marine Corps
The United States Marine Corps (USMC) was the procuring entity for the first-generation Harrier, receiving AV-8A models.
The British Aerospace Sea Harrier was specifically designed for what type of operations?
Answer: Naval operations from aircraft carriers.
The British Aerospace Sea Harrier is a naval variant of the V/STOL jet, configured for fighter, reconnaissance, and attack roles, and was operated by the Royal Navy and the Indian Navy from aircraft carriers.
The second generation of Harrier aircraft, known as the Harrier II, was a collaborative effort between which two companies?
Answer: British Aerospace and McDonnell Douglas
The second-generation Harrier II development was a collaborative effort between British Aerospace and McDonnell Douglas.
Which of the following Harrier variants was equipped with a radar system for air-to-air and air-to-surface targeting?
Answer: Sea Harrier FA2
The Sea Harrier FA2 variant was equipped with the Ferranti Blue Fox / Blue Vixen radar system, enabling air-to-air and air-to-surface targeting capabilities.
The Harrier II Plus configuration signifies the end of Harrier production, with the last aircraft delivered in:
Answer: 2003
The 'Harrier II Plus' configuration denotes the final batch of remanufactured aircraft, with the last delivery occurring in December 2003, signifying the conclusion of the Harrier production line.
Which country's navy operated the AV-8S Matador, a variant of the Harrier jump jet?
Answer: Spanish Navy
The Spanish Navy operated the AV-8S Matador, a variant of the Harrier jump jet.
Which of these was NOT an operator of the Harrier II or its variants, according to the provided text?
Answer: Royal Canadian Air Force
According to the provided information, current operators of Harrier II variants include the United States Marine Corps, the Spanish Navy, and the Italian Navy. The Royal Canadian Air Force is not listed as an operator.
What was the total number of Harriers of all types delivered by the end of production?
Answer: 824
The production of the Harrier family concluded with the delivery of a total of 824 aircraft across all variants.
The Sea Harrier played a minor role in the Falklands War due to its limited capabilities.
Answer: False
The Sea Harrier achieved significant prominence during the 1982 Falklands War, operating from the aircraft carriers HMS Invincible and HMS Hermes, indicating a major rather than minor role.
The Harrier can perform a vertical takeoff at its maximum loaded weight, provided it uses a short takeoff roll.
Answer: False
The Harrier's vertical takeoff capability is constrained to operations at less than its maximum loaded weight. Missions requiring a full complement of fuel and ordnance necessitate a short takeoff to augment vertical lift with aerodynamic forces.
'Vectoring in forward flight' (VIFFing) is a technique used to increase the Harrier's maximum speed.
Answer: False
'Vectoring in Forward Flight' (VIFFing) is a tactical maneuver wherein the Harrier's vectored thrust nozzles are rotated from their standard rearward orientation during forward flight. This technique facilitates abrupt deceleration and enhanced turn rates, not an increase in maximum speed.
The Harrier is considered 'forgiving' to fly due to its simple transition between conventional and VTOL flight modes.
Answer: False
The Harrier's flight characteristics are often described as 'unforgiving' due to the demanding nature of managing transitions between conventional wing-borne flight and VTOL/STOL modes, requiring considerable pilot skill and concentration.
The 'ski-jump ramp' is used to assist aircraft in achieving vertical landings on carriers.
Answer: False
The 'ski-jump ramp,' incorporated on the bows of certain aircraft carriers, serves to augment the Harrier's ability to achieve airborne status during short takeoffs by imparting an upward trajectory, thereby supplementing aerodynamic lift, not for vertical landings.
In which major conflict did the Sea Harrier FRS.1 play a significant and high-profile role?
Answer: Falklands War (1982)
The Sea Harrier achieved significant prominence during the 1982 Falklands War, operating from the aircraft carriers HMS Invincible and HMS Hermes, indicating a major rather than minor role.
What tactical maneuver involves rotating the Harrier's engine nozzles during forward flight to achieve sudden braking or higher turn rates?
Answer: Vectoring in Forward Flight (VIFFing)
'Vectoring in Forward Flight' (VIFFing) is a tactical maneuver wherein the Harrier's vectored thrust nozzles are rotated from their standard rearward orientation during forward flight. This technique facilitates abrupt deceleration and enhanced turn rates.
A key limitation of the Harrier's vertical takeoff capability is that it can only be performed:
Answer: At less than the maximum loaded weight.
The Harrier's vertical takeoff capability is constrained to operations at less than its maximum loaded weight. Missions requiring a full complement of fuel and ordnance necessitate a short takeoff to augment vertical lift with aerodynamic forces.
Why is flying the Harrier often described as 'unforgiving'?
Answer: Pilots must skillfully manage transitions between conventional and VTOL flight modes.
The Harrier's flight characteristics are often described as 'unforgiving' due to the demanding nature of managing transitions between conventional wing-borne flight and VTOL/STOL modes, requiring considerable pilot skill and concentration.
Joint Force Harrier was disbanded due to the introduction of new V/STOL technologies rendering it obsolete.
Answer: False
The Joint Force Harrier operational unit was dissolved in 2010 as part of a cost-reduction initiative, not due to obsolescence from new V/STOL technologies.
The F-35B Lightning II is the aircraft designated to replace the Harrier in several air forces and navies.
Answer: True
The F-35B variant of the F-35 Lightning II has been adopted to succeed V/STOL aircraft, including the Harrier, in the operational fleets of the United States Marine Corps, Royal Air Force, Royal Navy, and Italian Navy.
The Indian Navy replaced its Sea Harriers with the F-35B STOVL fighter.
Answer: False
The Indian Navy decommissioned its Sea Harrier fleet in 2016, subsequently integrating the conventional Mikoyan MiG-29K into its naval aviation arm, not the F-35B STOVL fighter.
The disbandment of Joint Force Harrier in 2010 was primarily attributed to:
Answer: Cost-saving measures implemented by the Ministry of Defence.
The Joint Force Harrier operational unit was dissolved in 2010 as part of a cost-reduction initiative, not due to obsolescence or the successful integration of the F-35B at that time.
The STOVL variant of the F-35 Lightning II, which replaced the Harrier in several services, is designated as:
Answer: F-35B
The F-35B variant of the F-35 Lightning II is specifically designed for Short Takeoff and Vertical Landing (STOVL) operations and has been adopted to succeed V/STOL aircraft, including the Harrier.