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ADS-33E-PRF
HANDLING QUALITIES REQUIREMENTS FOR MILITARY ROTORCRAFT
Organization:
ARMY - AV - Aviation and Missile Command
Year: 2000
Abstract: This specification contains the requirements for the flying and ground handling qualities of rotorcraft. It is intended that the specification should cover land based rotorcraft which have primary missions ranging from scout and attack to utility and cargo. Additional requirements or modified standards may be required for rotorcraft that have to operate from small ships in sea states resulting in more than small ship motion. Intended use is described in 6.1.
Application
The requirements of this specification are intended to assure that no limitations on flight safety or on the capability to perform intended missions will result from deficiencies in flying qualities. Flying qualities for the rotorcraft shall be in accordance with the provisions of this specification unless specific deviations are authorized by the Government. Additional or alternate special requirements may be specified by the procuring activity. For example, if the form of a requirement should not fit a particular vehicle configuration or control mechanization, the Government may, at its discretion, agree to a modified requirement that will maintain an equivalent degree of acceptability.Intended Use: This performance specification establishes requirements for the flying and ground handling qualities of military rotorcraft. It is intended that the specification should cover land-based rotorcraft that have primary missions ranging from scout and attack to utility and cargo. Additional requirements or modified standards may be required for rotorcraft that operate from small ships in sea states resulting in more than small ship motion. The requirements are intended for application in development of a new system, or for a major system upgrade. If met, they should assure that no limitations on flight safety, or on the capability to perform intended missions, will result from deficiencies in flying qualities. The criteria and MTEs can also be used as a development tool since they provide quantitative benchmarks and calibrated maneuver standards which may be valuable for assessing the need for upgrades, or for diagnosing the cause of deficient performance. Application of this specification to a specific system requires minimal tailoring. This tailoring basically consists of selecting the appropriate MTEs corresponding to the operational missions, and defining several aspects of the operational environment. All of the topics to be specified in the system specification have been gathered into 3.1. Guidance on tailoring these topics will be provided in a separate handbook.
Application
The requirements of this specification are intended to assure that no limitations on flight safety or on the capability to perform intended missions will result from deficiencies in flying qualities. Flying qualities for the rotorcraft shall be in accordance with the provisions of this specification unless specific deviations are authorized by the Government. Additional or alternate special requirements may be specified by the procuring activity. For example, if the form of a requirement should not fit a particular vehicle configuration or control mechanization, the Government may, at its discretion, agree to a modified requirement that will maintain an equivalent degree of acceptability.Intended Use: This performance specification establishes requirements for the flying and ground handling qualities of military rotorcraft. It is intended that the specification should cover land-based rotorcraft that have primary missions ranging from scout and attack to utility and cargo. Additional requirements or modified standards may be required for rotorcraft that operate from small ships in sea states resulting in more than small ship motion. The requirements are intended for application in development of a new system, or for a major system upgrade. If met, they should assure that no limitations on flight safety, or on the capability to perform intended missions, will result from deficiencies in flying qualities. The criteria and MTEs can also be used as a development tool since they provide quantitative benchmarks and calibrated maneuver standards which may be valuable for assessing the need for upgrades, or for diagnosing the cause of deficient performance. Application of this specification to a specific system requires minimal tailoring. This tailoring basically consists of selecting the appropriate MTEs corresponding to the operational missions, and defining several aspects of the operational environment. All of the topics to be specified in the system specification have been gathered into 3.1. Guidance on tailoring these topics will be provided in a separate handbook.
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| contributor author | ARMY - AV - Aviation and Missile Command | |
| date accessioned | 2017-09-04T16:19:15Z | |
| date available | 2017-09-04T16:19:15Z | |
| date copyright | 02/29/2000 | |
| date issued | 2000 | |
| identifier other | THOPJBAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho15137D83081DAC4261598F1EFDEC9FCD/handle/yse/82684 | |
| description abstract | This specification contains the requirements for the flying and ground handling qualities of rotorcraft. It is intended that the specification should cover land based rotorcraft which have primary missions ranging from scout and attack to utility and cargo. Additional requirements or modified standards may be required for rotorcraft that have to operate from small ships in sea states resulting in more than small ship motion. Intended use is described in 6.1. Application The requirements of this specification are intended to assure that no limitations on flight safety or on the capability to perform intended missions will result from deficiencies in flying qualities. Flying qualities for the rotorcraft shall be in accordance with the provisions of this specification unless specific deviations are authorized by the Government. Additional or alternate special requirements may be specified by the procuring activity. For example, if the form of a requirement should not fit a particular vehicle configuration or control mechanization, the Government may, at its discretion, agree to a modified requirement that will maintain an equivalent degree of acceptability.Intended Use: This performance specification establishes requirements for the flying and ground handling qualities of military rotorcraft. It is intended that the specification should cover land-based rotorcraft that have primary missions ranging from scout and attack to utility and cargo. Additional requirements or modified standards may be required for rotorcraft that operate from small ships in sea states resulting in more than small ship motion. The requirements are intended for application in development of a new system, or for a major system upgrade. If met, they should assure that no limitations on flight safety, or on the capability to perform intended missions, will result from deficiencies in flying qualities. The criteria and MTEs can also be used as a development tool since they provide quantitative benchmarks and calibrated maneuver standards which may be valuable for assessing the need for upgrades, or for diagnosing the cause of deficient performance. Application of this specification to a specific system requires minimal tailoring. This tailoring basically consists of selecting the appropriate MTEs corresponding to the operational missions, and defining several aspects of the operational environment. All of the topics to be specified in the system specification have been gathered into 3.1. Guidance on tailoring these topics will be provided in a separate handbook. | |
| language | English | |
| title | ADS-33E-PRF | num |
| title | HANDLING QUALITIES REQUIREMENTS FOR MILITARY ROTORCRAFT | en |
| type | standard | |
| page | 100 | |
| status | Active | |
| tree | ARMY - AV - Aviation and Missile Command:;2000 | |
| contenttype | fulltext |