Fracture control requirements have been developed to address damage tolerance of composites for manned space flight hardware. The requirements provide the framework for critical and noncritical hardware assessment and testing. The need for damage threat assessments, impact damage protection plans, and nondestructive evaluation are also addressed. Hardware intended to be damage tolerant have extensive coupon, sub-element, and full-scale testing requirements in-line with the Building Block Approach concept from the MIL-HDBK-17, Department of Defense Composite Materials Handbook
In aerospace engineering, a structural design has to account for Damage Tolerance (DT). A flawed str...
Aerospace structures comprised of composite materials are traditionally certified empirically via th...
A monograph is presented which establishes structural design criteria and recommends practices to en...
The certification experience for the primary, safety-of-flight composite structure applications on t...
This paper describes how the intent of current NASA fracture control requirements may be applied to ...
Objectives of customer mandated aircraft structural integrity initiatives in design are to guide mat...
Aerospace structures comprised of composite materials are traditionally certified empirically via th...
Damage tolerance consists of analysis and experimentation working together. Impact damage is usually...
Commercial transport aircraft operating in the United States are certified by the Federal Aviation A...
Use of lightweight composite materials in space and aircraft structure designs is often challenging ...
Aerospace vehicles are designed to be durable and damage tolerant. Durability is largely an economic...
The need for safe, lightweight, less expensive, and more reliable launch vehicle components is being...
The purpose of composite repair development at KSC (John F. Kennedy Space Center) is to provide supp...
Fracture toughness testing techniques for composite materials are reviewed for simplicity, applicabi...
Damage tolerance performance is critical to composite structures because surface impacts at relative...
In aerospace engineering, a structural design has to account for Damage Tolerance (DT). A flawed str...
Aerospace structures comprised of composite materials are traditionally certified empirically via th...
A monograph is presented which establishes structural design criteria and recommends practices to en...
The certification experience for the primary, safety-of-flight composite structure applications on t...
This paper describes how the intent of current NASA fracture control requirements may be applied to ...
Objectives of customer mandated aircraft structural integrity initiatives in design are to guide mat...
Aerospace structures comprised of composite materials are traditionally certified empirically via th...
Damage tolerance consists of analysis and experimentation working together. Impact damage is usually...
Commercial transport aircraft operating in the United States are certified by the Federal Aviation A...
Use of lightweight composite materials in space and aircraft structure designs is often challenging ...
Aerospace vehicles are designed to be durable and damage tolerant. Durability is largely an economic...
The need for safe, lightweight, less expensive, and more reliable launch vehicle components is being...
The purpose of composite repair development at KSC (John F. Kennedy Space Center) is to provide supp...
Fracture toughness testing techniques for composite materials are reviewed for simplicity, applicabi...
Damage tolerance performance is critical to composite structures because surface impacts at relative...
In aerospace engineering, a structural design has to account for Damage Tolerance (DT). A flawed str...
Aerospace structures comprised of composite materials are traditionally certified empirically via th...
A monograph is presented which establishes structural design criteria and recommends practices to en...