Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Radio Navigation Equipment Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Radio Navigation Equipment Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 11

ISBN-13:

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This specification covers the design, performance, and testing requirements for the radio navigation equipment for the supersonic transport aircraft. It is anticipated that PVDR capability may be a requirement for the SST airplane. This requirement could modify the description of the VHF navigation package which currently is planned to contain the VOR localizer and glide-slope functions. This specification covers the following radio navigation equipment: LF ADF, VHF navigation, Glide slope, Marker beacon and DME.

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Flight Instrumentation Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Flight Instrumentation Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 33

ISBN-13:

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This specification establishes the design, construction, performance requirements, and test objectives of the flight instrumentation equipment for the Model 733 supersonic transport. This specification covers the following flight instrumentation equipment: Attitude director indicator; Horizontal situation indicator; Flight director computer; Comparator warning and approach gate monitor; Approach progress annunciator; Radio magnetic indicator; Standby attitude/heading indicator; Radio altimeter; and Radar altitude/vertical speed indicator. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Inertial Navigation System Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Inertial Navigation System Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 18

ISBN-13:

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This specification establishes preliminary performance, design, and construction requirements applicable to the inertial navigation system for the supersonic transport. The requirements will be updated as the ARINC inertial navigation system characteristic is developed. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of the requirements to production airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Weather and Mapping Radar Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Weather and Mapping Radar Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 11

ISBN-13:

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The performance, design, construction, and test requirements specified are applicable to the weather and ground mapping radar equipment for the supersonic transport aircraft. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report) Air Induction System Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report) Air Induction System Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 15

ISBN-13:

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The specification describes and establishes the requirements and testing objectives for the air induction (inlet) system. Performance requirements established herein are design objectives to be applied to prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Hydraulic System Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Hydraulic System Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 20

ISBN-13:

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This specification describes and establishes the requirements and testing objectives for the hydraulic power, flight control, and utility actuation systems. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing.

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Air Data System Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Air Data System Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 45

ISBN-13:

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This specification defines preliminary performance, design, and construction requirements applicable to the air data system for the supersonic transport. The air data system is comprised of the following items: Pitot-static installation, Total temperature probe, Air data computer, Pressure altitude indicator, Airspeed indicator, Mach number indicator, Total temperature indicator, True airspeed indicator, Static air temperature indicator, and Angle-of-attack sensor. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Air Induction Control System Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Air Induction Control System Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 17

ISBN-13:

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This specification describes the system and establishes the testing requirements for the air induction hydraulic and control system. In the remainder of this document, the air induction system will be referred to as inlet system. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production-airplane design will be established after prototype flight testing. (Author).

Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Engine Inlet Anti-icing Performance Specification
Commercial Supersonic Transport Program. Phase Ii-c. Interim Aircraft Performance Assessment Report. Engine Inlet Anti-icing Performance Specification

Author: BOEING CO RENTON WA.

Publisher:

Published: 1965

Total Pages: 13

ISBN-13:

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This specification describes the engine inlet anti-icing system and establishes its requirements, and testing objectives. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be determined after prototype flight testing.