Aircraft And Space Vehicle Engineering Official British Standard

BS 2G 232:1987

Comprehensive British Standard for aircraft and space vehicle engineering. Ensures compliance, safety, and quality in aerospace design and manufacturing.

Comprehensive Aerospace Engineering Standard

BS 2G 232:1987 is a critical British Standard that provides detailed specifications and guidelines for the engineering of aircraft and space vehicles. Developed by industry experts, this standard ensures the highest levels of safety, quality, and compliance in the aerospace sector.

Comprehensive Aerospace Specifications

This standard covers a wide range of technical requirements for the design, manufacturing, and testing of aircraft and space vehicle components, including:

  • Structural integrity and load-bearing capacity
  • Aerodynamic performance and stability
  • Propulsion systems and fuel efficiency
  • Electrical and electronic systems
  • Environmental control and life support
  • Avionics and navigation equipment
  • Materials selection and testing
  • Quality assurance and inspection procedures

Ensuring Compliance and Safety

Compliance with BS 2G 232:1987 is essential for any organization involved in the design, manufacture, or maintenance of aircraft and space vehicles. By adhering to this standard, companies can:

  • Demonstrate adherence to industry-accepted best practices and safety protocols
  • Reduce the risk of accidents, failures, or malfunctions during operation
  • Ensure the airworthiness and reliability of their aerospace products
  • Meet regulatory requirements and obtain necessary certifications
  • Enhance their reputation and competitiveness in the global aerospace market

Comprehensive Technical Guidance

The BS 2G 232:1987 standard provides detailed technical specifications and guidelines across a wide range of aerospace engineering disciplines. This comprehensive resource covers:

Structural Design and Analysis

The standard outlines requirements for the structural design, analysis, and testing of aircraft and space vehicle components, ensuring they can withstand the extreme loads and stresses encountered during flight operations.

Aerodynamics and Flight Mechanics

This section addresses the aerodynamic performance, stability, and control characteristics of aerospace vehicles, helping designers optimize their designs for maximum efficiency and safety.

Propulsion and Power Systems

The standard covers the design, integration, and testing of propulsion systems, including engines, fuel systems, and power generation equipment, ensuring optimal performance and reliability.

Avionics and Electronics

The standard provides guidance on the design, installation, and testing of avionics, navigation, and other electronic systems, ensuring they meet stringent reliability and safety requirements.

Materials and Manufacturing

The standard specifies the selection, testing, and processing of materials used in aerospace applications, as well as the manufacturing processes and quality control measures required to ensure consistent, high-quality production.

By adhering to the comprehensive technical specifications and guidelines outlined in BS 2G 232:1987, aerospace organizations can ensure the safety, reliability, and compliance of their aircraft and space vehicle designs, helping to maintain the highest standards of quality and performance in the industry.

Technical Information

Aircraft And Space Vehicle Engineering
BSI Group
0 580 15920 5
Specification Details
  • Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation
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