ASTM E1997-15(2021) PDF
Standard Practice for the Selection of Spacecraft Materials
Standard Practice for the Selection of Spacecraft Materials
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 17
- Дата публикации:
- 1 сентября 2021 г.
- Издание:
- E1997
- ICS:
- 49.025.01
SIGNIFICANCE AND USE 3.1 This practice is a guideline for proper materials and process selection and application. The specific application of these guidelines must take into account contractual agreements, functional performance requirements for particular programs and missions, and the actual environments and exposures anticipated for each material and the equipment in which the materials are used. Guidelines are not replacements for careful and informed engineering judgment and evaluations and all possible performance and design constraints and requirements cannot be foreseen. This practice is limited to unmanned systems and unmanned or external portions of manned systems, such as the Space Station. Generally, it is applicable to systems in low earth orbit, synchronous orbit, and interplanetary missions. Although many of the suggestions and cautions are applicable to both unmanned and manned spacecraft, manned systems have additional constraints and requirements for crew safety which may not be addressed adequately in unmanned designs. Because of the added constraints and concerns for human-rated systems, these systems are not addressed in this practice. SCOPE 1.1 The purpose of this practice is to aid engineers, designers, quality and reliability control engineers, materials specialists, and systems designers in the selection and control of materials and processes for spacecraft, external portion of manned systems, or man-tended systems. Spacecraft systems are very different from most other applications. Space environments are very different from terrestrial environments and can dramatically alter the performance and survivability of many materials. Reliability, long life, and inability to repair defective systems (or high cost and difficultly of repairs for manned applications) are characteristic of space applications. This practice also is intended to identify materials processes or applications that may result in degraded or unsatisfactory performance of systems, subsystems, or components. Examples of successful and unsuccessful materials selections and uses are given in the appendices. 1.2 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM E1997-15(2021), Standard Practice for the Selection of Spacecraft Materials, provides essential guidelines for engineers, materials specialists, systems designers, and quality control professionals involved in choosing and controlling materials for spacecraft and related systems. Developed by ASTM International, this standard focuses on unmanned systems and the external portions of manned or man-tended systems, including usage in low Earth orbit, synchronous orbit, and interplanetary missions.
Selecting appropriate materials for spacecraft is fundamentally different from terrestrial applications, due to the unique challenges presented by space environments. These include extreme temperatures, vacuum conditions, radiation exposure, the risk of micrometeoroid impacts, and the presence of atomic oxygen. The standard aims to increase reliability, ensure long operational lifetimes, and mitigate the high cost and difficulty of repairs in space.
Key Topics
- Environmental Impact on Materials: Outlines how different orbital regions-low Earth orbit, synchronous orbit, and interplanetary space-impose specific constraints such as temperature extremes, radiation, debris, and atomic oxygen, each of which affects material selection and lifespan.
- Materials to Avoid: Advises against using substances known to perform poorly or degrade in space, including:
- Metals with high vapor pressure (e.g., mercury, cadmium, zinc)
- Pure tin, due to whisker growth and potential for electrical shorts
- Stress-corrosion-sensitive metals unless properly treated
- Materials with high outgassing or volatile emissions
- Compounds prone to particulate contamination or instability under thermal cycling
- Material Selection Process: Emphasizes that only careful, informed engineering judgment, supported by rigorous testing and documentation, is sufficient for spacecraft materials selection. The need to verify properties, control suppliers, and avoid reliance on simple data sheets is highlighted.
- Control Methods: Promotes the establishment of approved materials and process lists unique to each space mission, frequent testing of key properties, close oversight by experienced materials engineers, and integration of materials review in all design phases.
- Documentation and Traceability: Recommends materials lists and process specifications be strictly controlled, configuration-managed, and reviewed by qualified specialists to ensure only suitable, proven materials are used.
Applications
ASTM E1997-15(2021) is widely applicable in the aerospace industry, specifically for:
- Spacecraft Construction: Useful in selecting both structural and non-structural materials for satellites, probes, and external equipment on manned space stations.
- Subsystems and Components: Guides selection for critical subsystems such as thermal blankets, antennas, solar arrays, electrical connectors, and adhesives.
- Mission Planning: Aids in evaluating material durability and compatibility for projected mission environments, such as exposure to vacuum, radiation, or outgassing-sensitive payloads.
- Quality Assurance: Serves as a reference for the development of internal material control policies, supplier qualifications, and compliance verification strategies.
- R&D and Risk Mitigation: Essential for new design or experimentation, helping to avoid unsuccessful material choices and increase mission reliability.
Related Standards
ASTM E1997-15(2021) references and complements several important industry standards, including:
- ASTM E595 - Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum
- MIL-STD-889 - Dissimilar Materials
- MIL-HDBK-5 - Metallic Materials and Elements for Aerospace Vehicle Structures
- MIL-HDBK-17 - Properties of Composite Materials
- ESA PSS-07/QRM-0 - European Space Agency Guidelines for Space Materials Selection
- QQ-A-250 - Federal Specification for Aluminum and Aluminum Alloy Plate and Sheet
These standards collectively help ensure that spacecraft materials are selected based on robust, reliable criteria, improving the long-term success and safety of aerospace missions.
Keywords: spacecraft materials, selection guidelines, ASTM E1997, space environment, outgassing, vacuum, radiation, quality control, aerospace materials, materials testing, approved process lists, unmanned systems, low Earth orbit materials, synchronous orbit, interplanetary missions.
Технические детали
- Технический комитет
- E21 - Space Simulation and Applications of Space Technology
- SKU
- ASTM E1997-15(2021)
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