REG NASA-LLIS-0643--2000 Lessons Learned NASA Preferred Reliability Practices Design and Test Practices for Aerospace Systems Environmental Factors.pdf
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1、Best Practices Entry: Best Practice Info:a71 Committee Approval Date: 2000-02-18a71 Center Point of Contact: GRCa71 Submitted by: Wil HarkinsSubject: NASA Preferred Reliability Practices; Design and Test Practices for Aerospace Systems; Environmental Factors Practice: At the onset of the design proc
2、ess, identify the operating conditions that will be encountered during the life of the equipment.Programs that Certify Usage: Programs That Certified Usage: Space Electronic Rocket Test (SERT) I and II, Communication Technology Satellite (CTS), ACTS, Space Experiments, Launch Vehicles, Space Power S
3、ystems, and Space Station Freedom.Center to Contact for Information: GRCImplementation Method: This Lessons Learned is based on Reliability Practice NO. PD-EC-1101 from NASA Technical Memorandum 4322A, NASA Preferred Reliability Practices for Design and Test.Benefits:Each of the identified environme
4、ntal factors requires consideration in the design process. This assures that adequate environmental strength is incorporated into the design to ensure reliability.Implementation Method:Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-To ensure a relia
5、bility-oriented design, determine the needed environmental resistance of the equipment. The initial requirement is to define the operating environment for the equipment. A Life-Cycle Environment Profile, containing this information, should be developed.A Life-Cycle Environment Profile is a forecast
6、of events and associated environmental conditions that an item experiences from manufacturing to retirement. The life cycle includes the phases that an item will encounter such as: handling, shipping, or storage prior to use; disposition between missions (storage, standby, or transfer to/from repair
7、 sites); geographical locations of expected deployment; and platform environments. The environment or combination of environments the equipment will encounter at each phase should be determined. All deployment scenarios should be described as a baseline to identify the environments most likely to be
8、 associated with each life cycle phase. The following factors should also be taken into account:a. Hardware configuration.b. Environment(s) that will be encountered.c. Platform/hardware interfaces.d. Interfaces with other equipment.e. Absolute and relative duration of exposure phase.f. Probability t
9、hat environmental condition(s) will occur.g. Geographical locations.h. Any other information that will help identify environmental conditions that may impact the item.The steps in developing a Life-Cycle Environment Profile are as follows:1. Describe anticipated events for an item of equipment, from
10、 final factory acceptance through terminal expenditure or removal from inventory.2. Identify significant natural and induced environments or combination of environments for each anticipated shipping, storage, and logistic event (such as transportation, dormant storage, stand-by, bench handling, and
11、ready modes, etc.).3. Describe environmental and stress conditions (in narrative and statistical form) to which equipment will be subjected during the life cycle. Data may be derived by calculation, laboratory tests, or operational measurements. Estimated data should be replaced with actual values a
12、s determined. The profile should show the number of measurements used to obtain the average value of these stresses and design achievements as well as their variability (expressed as standard deviation).This analysis can be used to: develop environmental design criteria consistent with anticipated P
13、rovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-operating conditions, evaluate possible effects of change in environmental conditions, and provide traceability for the rationale applied in criteria selection for future use on the same program or other
14、 programs.A listing of typical environmental factors is included in Table 1.Table 1: Environmental Coverage Checklist (Typical) Natural InducedAlbedo, Planetary IRCloudsElectromagnetic RadiationElectrostatic DischargeFogFreezing RainFrostFungusGravity, LowHailHumidity, HighHumidity, HightIceIonized
15、GasesLightningMagnetics, GeoMeteoroidsPollution, AirPressure, HighPressure, Low, VacuumRadiation, Cosmic, SolarRainSalt SpraySand and DustSleetSnowTemperature, HighTemperature, LowWindAccelerationChemicalsCoronaElectromagnetic, LaserElectromagnetic RadiationElectrostatic DischargeExplosionIcingMagne
16、ticsMoistureNuclear RadiationShock, Pyro, ThermalSpace DebrisTemperature, High, Aero. Heating, FireTemperature, Low, Aero. CoolingTurbulenceVapor TrailsVibration, Mechanical, MicrophonicsVibration, AcousticTechnical Rationale:Provided by IHSNot for ResaleNo reproduction or networking permitted witho
17、ut license from IHS-,-,-Given the dependence of equipment reliability on the operating conditions encountered during the life cycle, it is important that such conditions be identified accurately at the beginning of the design process. Environmental factors that strongly influence equipment reliabili
18、ty are included in Table 1, which provides a checklist for environmental coverage (typical).Concurrent (combined) environments may be more detrimental to reliability than the effects of a single environment. In characterizing the design process, design/test criteria must consider both single and/or
19、combined environments in anticipation of providing the hardware capability to withstand the hazards identified in the system profile. The effects of typical combined environments are illustrated in a matrix relationship in Figure 1, which shows combinations where the total effect is more damaging th
20、an the cumulative effect of each environment acting independently. For example, an item may be exposed to a combination such as temperature, humidity, altitude, shock, and vibration while it is being transported. The acceptance to end-of-life history of an item must be examined for these effects. Ta
21、ble 2 provides reliability considerations for pairs of environmental factors.Each environmental factor that is present requires a determination of its impact on the operational and reliability characteristics of the materials and parts comprising the equipment being designed. Packaging techniques sh
22、ould be identified that afford the necessary protection against the degrading factors.In the environmental stress identification process that precedes selection of environmental strength techniques, it is essential to consider stresses associated with all life intervals of the equipment. This includ
23、es operational and maintenance environments as well as the pre-operational environments, when stresses imposed on the parts during manufacturing assembly, inspection, testing, shipping, and installation may have significant impact on equipment reliability. Stresses imposed during the pre-operational
24、 phase often are overlooked; however, they may represent a particularly harsh environment that the equipment must withstand. Often, the environments to which systems are exposed during shipping and installation are more severe than those encountered during normal operating conditions. It is probable
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