BS EN 2355:1989

Comprehensive Aircraft and Space Vehicle Engineering Standard

Ensure your aircraft and space vehicle designs meet the highest international engineering standards with BS EN 2355:1989. This British Standard, identical to EN 2355:1988, provides detailed technical specifications and requirements for the engineering of aircraft and space vehicles.

Key Features and Benefits:

• Comprehensive coverage of aircraft and space vehicle engineering principles
• Aligned with EN 2355:1988 to support international compliance
• Detailed technical specifications across 12 sections
• Authoritative guidance from the British Standards Institution (BSI)
• Available in PDF digital format or printed hardcopy

Detailed Technical Specifications

BS EN 2355:1989 covers a wide range of technical requirements for the engineering of aircraft and space vehicles. The standard is structured across 12 key sections:

1. General Requirements

Outlines fundamental principles and general requirements for aircraft and space vehicle engineering, including design, materials, and manufacturing processes.

2. Structural Design

Provides detailed specifications for the structural design of aircraft and space vehicle components, including load calculations, stress analysis, and safety factors.

3. Aerodynamics

Covers the aerodynamic design of aircraft and space vehicles, including airflow analysis, lift and drag calculations, and stability requirements.

4. Propulsion Systems

Specifies the engineering requirements for aircraft and space vehicle propulsion systems, such as engines, thrusters, and fuel systems.

5. Electrical Systems

Outlines the technical specifications for the electrical systems of aircraft and space vehicles, including power generation, distribution, and control.

6. Avionics and Instrumentation

Covers the engineering requirements for the avionics and instrumentation systems used in aircraft and space vehicles, including navigation, communication, and control systems.

7. Environmental Control

Provides specifications for the environmental control systems of aircraft and space vehicles, such as temperature, pressure, and humidity regulation.

8. Life Support Systems

Outlines the engineering requirements for the life support systems used in space vehicles, including oxygen supply, water purification, and waste management.

9. Landing Gear

Covers the technical specifications for the landing gear systems of aircraft, including design, materials, and performance requirements.

10. Maintenance and Servicing

Specifies the engineering requirements for the maintenance and servicing of aircraft and space vehicles, including accessibility, inspection, and repair procedures.

11. Testing and Verification

Outlines the testing and verification procedures required to ensure the compliance and performance of aircraft and space vehicle engineering designs.

12. Documentation and Certification

Provides guidance on the documentation and certification requirements for aircraft and space vehicle engineering, including technical reports, design drawings, and regulatory approvals.

By adhering to the comprehensive technical specifications outlined in BS EN 2355:1989, you can ensure that your aircraft and space vehicle engineering designs meet the highest international standards and support the safe and reliable operation of these critical systems.