Mission Range Sample Clauses
The Mission Range clause defines the specific geographic area or operational scope within which a party, typically in a defense or aerospace contract, is authorized to conduct missions or activities. This clause outlines the boundaries—such as coordinates, regions, or airspace—where operations like testing, training, or deployment may occur, and may include restrictions or conditions for entering or exiting the designated range. Its core function is to ensure all parties are clear on where activities are permitted, thereby preventing unauthorized operations and reducing the risk of legal or safety issues.
Mission Range. The still air range with a [*] pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee value:
Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED] kg over a guaranteed still air stage distance of not less than [DELETED] nautical miles when operated under the conditions defined below:
3.1.1 The departure airport conditions are such as to allow the required take-off weight to be used without any restriction. The destination airport conditions are such as to allow the required landing weight to be used without any restriction.
3.1.2 An allowance of [DELETED] of fuel is included for engine start and taxi-out at departure airport.
3.1.3 An allowance of [DELETED] kg of fuel is included for take-off and climb to [DELETED] ft above the departure airport with acceleration to climb speed in ISA conditions.
3.1.4 Climb from [DELETED] ft above the departure airport up to optimum cruise altitude using maximum climb thrust, cruise at a fixed Mach number of [DELETED] at a pressure altitude of [DELETED] ft, / [DELETED] ft, and descent to [DELETED] ft above the destination airport are conducted in ISA conditions. Climb and descent speeds below [DELETED] ft shall be [DELETED] knots CAS.
3.1.5 An allowance of [DELETED] kg of fuel is considered for approach and landing at destination airport.
3.1.6 An allowance of [DELETED] kg of fuel is considered for taxi in at the destination airport.
Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED] kg over a guaranteed still air stage distance of not less than [DELETED] nautical miles when operated under the conditions defined below:
3.1.1 The departure airport conditions are such as to allow the required take-off weight to be used without any restriction. The destination airport conditions are such as to allow the required landing weight to be used without any restriction.
3.1.2 An allowance of [DELETED] kg of fuel is included for engine start and taxi-out at departure airport.
3.1.3 An allowance of [DELETED] kg of fuel is included for take-off and climb to [DELETED] ft above the departure airport with acceleration to climb speed in ISA conditions.
Mission Range. The still air range with a *** pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles Conditions and operating rules: Still Air Range: The still air range is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is ***. The takeoff gross weight is *** the airport conditions. The takeoff gross weight shall conform to FAA Regulations.
Mission Range. The still air range with a *** pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles Conditions and operating rules: Still Air Range: The still air range is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is ***. The takeoff gross weight is *** the airport conditions. The takeoff gross weight shall conform to FAA Regulations. Climbout Maneuver: Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while climbing to *** feet above the departure airport altitude and retracting flaps and landing gear.
Mission Range. The Aircraft shall be capable of carrying a Zero Fuel Weight of [DELETED]kg over a guaranteed still air stage distance of not less than [DELETED]nautical miles when operated under the conditions defined below:
3.1.1 The departure airport conditions are such as to allow the required take-off weight to be used without any restriction. The destination airport conditions are such as to allow the required landing weight to be used without any restriction.
Mission Range. The still air range with a *** pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: *** Nautical Miles TOLERANCE: *** Nautical Miles GUARANTEE: *** Nautical Miles Conditions and operating rules: Still Air Range: The still air range is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent. Takeoff: The airport altitude is ***. The takeoff gross weight is *** the airport conditions. The takeoff gross weight shall conform to FAA Regulations. Climbout Maneuver: Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while climbing to *** feet above the departure airport altitude and retracting flaps and landing gear. P.A. No. 3860 AERO-B-BBA4-M09-0774C SS09-0285 Attachment A2 UAL-PA-03860-LA-1209430 Trent 1000-*** Engines Climb: The Aircraft climbs from *** feet above the departure airport altitude to *** feet altitude at *** KCAS. The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum block fuel. The climb continues at the recommended climb speed for minimum block fuel until *** Mach number is reached. The climb continues at *** Mach number to the initial cruise altitude. The temperature is standard day during climb. Maximum climb thrust is used during climb. Cruise: The Aircraft cruises at *** Mach number. The initial cruise altitude is *** feet. A step climb or multiple step climbs of *** feet altitude may be used when beneficial to minimize fuel burn. The temperature is standard day during cruise. The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may be used.
Mission Range. The still air range with a * pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee value: NOMINAL: * Nautical Miles TOLERANCE: * Nautical Miles GUARANTEE: * Nautical Miles Conditions and operating rules: