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spacebert_ecss | Each slave node shall implement the objects listed in Table 8-1 in its Object Dictionary. |
spacebert_ecss | For wire bonding or adhesive bonding soft gold shall be used. |
spacebert_ecss | For each telecommand packet transporting a request to change the maximum transition reporting delay, the application data field shall have the structure specified in Figure 8-113. |
spacebert_ecss | The data hold time after the DATA_CLK_OUT falling edge, tdh, shall be not less than 0. |
spacebert_ecss | The risk assessment shall cover the following: 1. a summary and description of each hazardous activity, 2. an assessment of the risks associated with the hazard, its likelihood and severity, 3. an identification of all risk reduction measures and the verification of their effectiveness after implementation, 4. a clear indication of the remaining and acceptable risks to operate the facility, 5. the methodology used for the risk assessment. |
spacebert_ecss | Swage-type terminals that are mounted in a plated-through hole shall be secured to the PCB by an elliptical funnel swage in accordance with Figure 8-6 (b). NOTE An elliptical funnel swage enables complete filling of the plated-through hole with solder. |
spacebert_ecss | The supplier shall ensure that inspection, measuring and test facilities, including both test hardware and test software are protected against adjustments, which can invalidate the calibration setting. |
spacebert_ecss | Each request to load raw memory data areas by reference shall contain: 1. if the raw data memory management subservice manages more than one memory, the identifier of the memory; 2. the file path of the file containing the data to load; 3. an ordered list of one or more instructions to load a raw memory data area by reference. |
spacebert_ecss | The interface between the space segment element and the launch facility shall be verified before actual spacecraft operation. |
spacebert_ecss | To summary-report the content of each packet store, N shall be set to 0. |
spacebert_ecss | Fluorescent dye should be used for potting of the rigid-to-flex interface. |
spacebert_ecss | The MMDD should include the following topics: 1. justification of used element types, spring and rigid connections, rigid body and relationships; 2. model adequacy to study specific structure behaviour (e.g. non-linear phenomena, local-global buckling, and contact); 3. model limitations (e.g. limitation on type of analyses can be performed or on output can be found); 4. significant model output: stress, frequencies. |
2005_phin_PURE | The following requirements describe baseline functionality for any system(s) implemented to support Outbreak Management: 2.1 System Architecture: Broad system-level needs, such as flexible configuration, should be addressed by systems supporting OM. 2.2 Data Requirements: Systems supporting OM need a variety of data to support investigations, including data regarding demographics, cases, exposures, investigations, agents, contacts, specimen/sample collection, laboratory tests, travel and conveyance, and restriction monitoring. 2.3 System Functions and Behaviors: Systems supporting OM should support case investigation, maintain detailed and comprehensive linkages, trace contacts, and quarantine and isolation monitoring activities. 2.4 Analysis, Visualization, and Report Generation: Systems supporting OM should enable investigators to produce both aggregated and individual reports about affected entities and events. 2.5 System Integration and Data Exchange: OM information must be exchangeable, based on established standards, between systems involved in the investigation, identification, confirmation, and reporting of a health event. 2.6 Vocabulary Standards: Standard vocabulary lists and data structures have been defined by standards organizations. Where they exist, systems supporting OM should use them. As additional standards are defined, they should be accepted and implemented 2.7 Operations: Personnel, roles, activities, and responsibilities necessary to support all aspects of OM should be clearly defined. 2.8 System Security and Availability: Security of OM data includes the protection of data from corruption and access by unauthorized individuals, as well as the protection of the actual systems supporting OM from sabotage or other failure. A plan must be established for continuing activities when systems supporting OM are unavailable. 2.9 Privacy: Patients, organizations, and personnel must be protected from fraudulent and unauthorized use of their information. |
2008_earthcare_web | The mechanical design of the satellite shall ensure that no loss of alignment which jeopardises or degrades the mission objectives can be caused by the action of applied loads (e.g. launch loads, deployment loads, thermal and moisture release). |
0000_mss_WEB | All the elements installed of the system shall be installed in such a way that they are protected against damage during a rough terrain drive |
spacebert_ecss | For any component that is estimated to have on-orbit performance degradation due to TID, a WCA of the function shall be performed in accordance with requirements of ECSS-Q-ST-30 to demonstrate that the function performs within specification despite radiation induced drifts in its constituent part parameters at EOL. |
2011_dot_WEB | The Core System subsystems shall accept time of day from the Time Subsystem |
2005_skal1_WEB | The SKA1_Mid central beam-former shall be able to form beams or more beams for one to sixteen sub-arrays independently and concurrently. |
spacebert_ecss | Contamination of painted surfaces shall be prevented. |
2006_hgs_ird_web | The MOC shall make available to the HSC the instrument memory image corresponding to an instrument memory dump requested by an ICC. |
2021_tmt_oad_WEB | The WFOS wavelength range shall be 0.31 - 1.0 碌m. |
2008_earthcare_web | Each instrument shall be designed to accept, from platform level, separate sources to be powered during instrument nominal operational modes and to power instrument (survival) heaters during non-operative and contingency situations. |
spacebert_ecss | The preparation of the silicon wafers聮 witnesses shall be performed as follows: 1. Using gloves and tweezers take one new or just cleaned silicon wafer. 2. Visually inspect the silicon wafer surface and edge conditions. (a) In case of edge damages, the silicon wafer is rejected. (b) In case of particulate or non-particulate matter, or a combination of both, visible on the surface, the silicon wafer is re-clean. 3. Place silicon wafer in the container. 4. Perform a background measurement with the microscope counting method (see 5.3). 5. Close the container. |
spacebert_ecss | In case of launch abort, the following shall be performed: 1. the propulsion system reset to a safe condition; 2. cryogenic propulsion systems drained and flushed. |
spacebert_ecss | The TCS interface control document shall list mechanical interface data including: 1. Dimensions, mass, material and surface properties of thermal hardware 2. Quality of thermally relevant surfaces NOTE For example: Roughness, flatness. 3. Properties of thermally relevant components, which are under the responsibility of other subsystems NOTE For example: Brackets, face sheets of sandwich. 4. Subsystem mass budget. |
spacebert_ecss | The selected cleaning materials, equipment and process conditions shall be listed. |
2008_keepass_PURE | This feature adds a new entry on the database. |
2018_jpss_l0_web | The algorithm shall produce a CO2 product that has a measurement range of 300 to 500 ppmv (Note 1). |
spacebert_ecss | Dies, setting of controls for the length of strip in automatic stripping machines and the selection of specific locators or positioners for crimping tools, shall be selected to meet process requirements. |
spacebert_ecss | Except for explicitly agreed single point failures, the capability shall be provided to recover all on-board functions after a single failure within a specific function. |
spacebert_ecss | The failure of the item shall not result in the release of any part or fragment which can create a catastrophic or critical hazard. NOTE For payloads on the NSTS or ISS, including transportation events to ISS, as minimum the mass and momentum limits defined in 6.1e are used. More in general, the maximum acceptable mass and velocity of released items is based on the results of the hazard analysis. |
spacebert_ecss | The supplier shall notify the customer of the non conformance details. |
2000_nasax38_PURE | The scheduler shall [SRS181] set the 50 Hz interval timer to a count down value so as to cause the next minor frame interrupt at 20 msec from the previous interrupt congruently in all operational FCPs. |
spacebert_ecss | The process parameters specified in the requirement 5.5.1d shall be defined in the process specification. |
2005_skal1_WEB | The interface between MeerKAT and SKA1_INFRA shall be compliant with SKA-TEL.AIV.SE- TEL.INFRA.SE-ICD-001 Interface Control Document |
2019_jpss_dps | The Sea Surface Temperature product shall provide sea surface temperatures with a measurement accuracy of 0.5 kelvin over the measurement range of the instrument. |
spacebert_ecss | The test equipment shall be as follows: 1. Signal generators, 2. Power amplifiers, 3. Receive antennas, (a) under 1 GHz, not applicable. (b) 1 GHz to 18 GHz, double ridge horn, 24.2 by 13.6 cm opening. NOTE Above 1 GHz receive antennas may be not used, see 5.4.11.3b.2. 4. Linearly polarized transmit antennas NOTE The following antennas are commonly used: 路 30 MHz to 200 MHz, biconical, 137 cm tip to tip, 路 200 MHz to 1 GHz, double ridge horn, 69,0 cm by 94,5 cm opening, or log-periodic, 路 1 GHz to 18 GHz, double ridge horn, 24,2 cm by 13,6 cm opening. 5. Electric field sensors (physically small - electrically short), 6. Measurement receiver, 7. Power meter, 8. Directional coupler, 9. Attenuator, 10. Data recording device, 11. LISN defined in 5.2.4, optional. |
spacebert_ecss | For each valid instruction to report a diagnostic parameter report structure, the diagnostic reporting subservice shall generate a single diagnostic parameter report structure report that contains exactly one diagnostic parameter report structure notification that includes: 1. the diagnostic parameter report structure identifier; 2. the periodic generation action status; 3. the collection interval; 4. the ordered list of simply commutated parameters; 5. the ordered list of super commutated parameter sets. |
2012_d51_web | The SICCI System shall take as input, data from the following primary SIC product: MODIS |
spacebert_ecss | The SVR shall present in gathering all the specific verification reports that have been planned to be provided w.r.t. the SVerP, including e.g.: 1. Traceability (when not already included in related software validation specification), presenting the following traceability matrices: 路 software validation specifications to TS 路 software validation specifications to RB 2. Feasibility, presenting in gathering all the specific verification reports that have been planned to be provided w.r.t. the SVerP, including e.g.: 路 Verification of software validation w.r.t. TS as per 5.8.3.8a. 路 Verification of software validation w.r.t. RB as per 5.8.3.8b. 路 Verification of software documentation as per 5.8.3.10 路 Verification of testing as per ECSS-Q-ST-80 clause 7.2.3.6 |
spacebert_ecss | The limits used for the qualification of elements and interfaces shall conform to the specified reliability and confidence. |
spacebert_ecss | The Redundancy Master shall command slave nodes that have performed a bus switch as defined in 8.3.3e into operational mode. |
spacebert_ecss | After soldering, the sample shall be allowed to cool down for at least 30 s. |
spacebert_ecss | The AR-N shall include a description and a discussion of the analysis methodology, describing what is done and why. |
spacebert_ecss | The calculated event rates shall be such that the application meets the projected availability, performance and reliability requirements. |
spacebert_ecss | The FMEA/FMECA performed at system level in phase C/D shall be utilized as support to diagnostic activities (in-flight and on ground) in order to support the system maintenance and restoring. |
2004_hp_srs_web | The cryocover in its open position shall be taken into account in straylight and thermal analysis. |
2012_marcopolo_WEB | The sampling spacecraft shall accommodate the ERC in a safe location such that the risk of collision of the ERC Thermal Protection System with the asteroid surface is minimized. |
spacebert_ecss | Each telemetry packet transporting a packet store content summary report shall be of message subtype 13. |
spacebert_ecss | The risk management policy document shall provide application guidance for each of the risk management functions in the process allowing the project聮s risk management organization flexibility while ensuring a common and coordinated approach to risk management and the coherence of the responsibilities and interfaces within the risk management process. |
2018_jpss_l0_web | The algorithm shall produce a bi-weekly vegetation indices product with a measurement precision of 0.04 NDVI units for NDVITOC. (Note 2) (Note 4) |
spacebert_ecss | To add all structure identifiers to the diagnostic parameter report storage-control configuration, N2 shall be set to 0. |
spacebert_ecss | Traceability of PFCI and the materials they are made of shall be implemented in conformance with ECSS-Q-ST-20 to provide assurance that: 1. The material used in the manufacture of structural hardware has properties fully representative of those used in the analysis or verification tests. 2. Structural hardware is manufactured and inspected in conformance with the specific requirements for the implementation of the fracture control programme. |
spacebert_ecss | The supplier shall examine the longitudinal microsections at a magnification of 脳50 for evidence of stress-corrosion cracking. |
1999_dii_PURE | Defense Information Infrastructure (DII), Shared Data Environment (SHADE), CAPSTONE DOCUMENT Version 1.0, 11 July 1996 ACCS-A1-100-006 System Specification for ATCCS, 22 March 1995 ATCCS-A1-302-001A Army Tactical Command and Control System Common ATCCS Support Software (CASS) Systems/Segment Specification CDRL A142 AWIS Software Requirements Specification (ASRD), July 1992 CDRL ML03 AWIS Systems Management Manual (SMM), 31 Oct. 1994 AWIS Support Software Design Document, December 1994 D18664A Standard Theater Army Command and Control System (STACCS) System Design Document Version 1.1/As Built, 1 Oct. 93 AAN-SDA001A Standard Theater Army Command and Control System (STACCS) System Specification, Version 1.1/As Built, 1 Oct. 93 Standard Theater Army Command and Control System (STACCS) System Software Programmers Manual, Draft. Global Command and Control System (GCCS) Integration Standard, Version 1.0, October 1994. Global Command and Control System (GCCS) Common Operating Environment Baseline, DISA, 28 November1994. User Interface Specifications for Global Command and Control System (GCCS), Version 1.0, October 1994. Draft Architectural Design Document for the Global Command and Control System (GCCS) Common Operating Environment (COE), Version 3, 24 July, 1994. |
spacebert_ecss | User populations and organisational requirements shall be specified and fed into the system requirements for the subsequent phases. NOTE These requirements are derived from the specified context of use (preliminary TA). |
spacebert_ecss | To report that no event definition for the related application process is in the event report blocking forward-control configuration, N2 shall be set to 0. |
spacebert_ecss | In a 3D figure, the axes above, within and below a plane shall be differentiated. |
0000_mss_WEB | The MTBF of daylight camera shall be not less than 10 000 h. |
spacebert_ecss | For specimens with a transverse weld, the specimen gauge length shall be equal or greater than the weld heat affected zone (HAZ). NOTE 1 When testing specimens with a transverse weld, note that the strain distribution within the HAZ varies as a function of the distance from the weld centre line. This implies that elongation varies as a function of the gauge length. NOTE 2 Weldments are characterized by non-uniformity in tensile properties. |
spacebert_ecss | The following constraints shall be assessed: 1. requirements originating from the initial technical specification. 2. programmatic project requirements and conditions. |
spacebert_ecss | The supplier shall evaluate and assess the CI control measures and implementation methods with respect to their effectiveness and feasibility by: 1. Selecting the CI control measures and implementation methods. 2. Defining a CI control strategy by prioritising the implementation of CI control. 3. Assessing the impact of CI control on project resources including risks during the associated decision making and selection process. 4. Assessing the impact of the implementation of CI control measures on the acceptability of risks associated with the critical items. |
spacebert_ecss | The term 聯coupon Bn聰 shall indicate all coupons B1, B2 聟 Bn for all plating sequences. |
spacebert_ecss | Unit accompanying documentation shall include the EIDP and, attached to the outside of the shipping container, the handling and packing or unpacking procedure and the safety procedures. |
spacebert_ecss | The test vehicle shall be microsectioned at the rigid-flex interface and at the zone that was bend during the test. |
spacebert_ecss | Test results used in analysis shall be summarized and reference test documentation shall be indicated. |
spacebert_ecss | Dependability lessons learnt shall be collected during the project life cycle including operational and disposal phases. |
spacebert_ecss | The virtual channel buffer that is ready and which has the highest precedence shall be permitted to send the next data segment. |
2005_clarushigh_PURE | The Clarus system shall have a minimum of one system administrator. |
spacebert_ecss | The FMEA/FMECA report shall include block diagrams and schematics to assist in describing the product, provide schematic diagrams, functional block diagrams and reliability block diagrams (RBDs) to a level consistent with the depth of the analysis and with design maturity. NOTE Functional tree is also useful to describe functional relationships. |
2012_stequest_mrd_web | The TTC-link shall support range and range-rate measurements. |
spacebert_ecss | Availability at a specific time shall be computed considering the mission loss probability. |
spacebert_ecss | The software product assurance plan shall be either a standalone document or a section of the supplier overall product assurance plan. |
2006_hgs_ird_web | The HSC shall make available to the MOC the instrument SSO avoidance angles. |
2004_hp_srs_web | The spacecraft shall accommodate the Planck telescope and its reflectors defined in AD1-3 and AD2-2 and shall provide the resources to ensure that the performance requirements of Planck and the needs |
spacebert_ecss | The supplier shall retain the quality records for at least ten years or in conformance with project business agreement requirements, and in conformance with the Test result sheet - DRD in Annex A. |
spacebert_ecss | The individual wire specification of silver-plated wires shall be applied for requirements other than the ones specified in 4.3.15.5a, b, c and d. |
2019_jpss_dps | The Vegetation Health Index Suite shall provide vegetation indices with a refresh every 7 days. |
spacebert_ecss | Surface, edge or corner cracks shall not be present on a coverglass. NOTE For further information, see MIL-PRF-13830. |
spacebert_ecss | For each valid instruction to add all structure identifiers to the diagnostic parameter report forward-control configuration, the real-time forwarding control subservice shall: 1. add, for the specified application process identifier, a diagnostic parameter report forward-control definition if not already existing; 2. delete, if any, all diagnostic parameter report structure identifiers of the related diagnostic parameter report forward-control definition. |
spacebert_ecss | The supplier shall verify with the OTS item manufacturer the design margins, and prefer those determined by test. |
2021_jpss2_web | Bits 5-15 of the Packet Primary Header shall contain the APID. |
spacebert_ecss | The supplier shall ensure that non-hermetically sealed materials of components meet the requirements of ECSS-Q-ST-70 regarding off-gassing, out-gassing, flammability, toxicity and any other criteria specified for the intended use. |
spacebert_ecss | Each instruction to delete the time-based scheduled activities identified by a filter shall contain the filter to identify the scheduled activities to delete consisting of: 1. a time window, consisting of: (a) the type of the time window that is one of "select all", "from time tag", "to time tag", "from time tag to time tag"; (b) for "from time tag" and "from time tag to time tag", the from time tag; (c) for "to time tag" and "from time tag to time tag", the to time tag; 2. if sub-schedules are supported, zero or more sub-schedules; 3. if groups are supported, zero or more groups. |
2005_claruslow_PURE | QEDS shall uniquely identify environmental data subscriptions. |
spacebert_ecss | For all data signals producing a square wave baseband PCM waveform, the symbol asymmetry measured at 50 % of the peak-to-peak amplitude point shall not exceed 1 % with the symbol asymmetry defined as follows: where long and short symbol refers to the duration of the long and short symbols |
spacebert_ecss | The following management parameters should be provided to configure, control and monitor the physical layer. 1. Enable line driver (port), which when set enables the line driver of the specified port so that it can transmit information. 2. Enable line receiver (port), which when set enables the line receiver of the specified port so that it can receive information. 3. Connector type and pin out for each connector. |
spacebert_ecss | The mechanical reference frames for the spacecraft, adapter and launch vehicle should be parallel and have the same positive direction. |
spacebert_ecss | If the subservice provides checksumming, then once the data related to an instruction to load an object memory data has been written to the memory, the structured data memory management subservice shall: 1. calculate the checksum of the loaded data; 2. compare it to the checksum value in that instruction; 3. if that checksum comparison fails: (a) immediately abort the execution of the related request; (b) generate a failed execution notification for that instruction. |
spacebert_ecss | The tank volume shall be determined at the extreme temperature and pressure ranges. |
2013_loft_mrd_web | The uplink and downlink data rates shall be compatible with the data transmission requirements during all mission phases. |
spacebert_ecss | The system shall be able to manage check-in/check-out, multiple versions. |
spacebert_ecss | For grounding spot resistance, in conformance with clause 5.5.3.3.4, the SCD-PVA shall state: 1. The maximum value, in W, of the resistance of bleed resistor lead (+) to substrate (-). 2. The maximum value, in W, of the grounding spots (+) to substrate (-). |
spacebert_ecss | All pressurized systems in NSTS and ISS payloads shall be in conformance with the requirements of NSTS 1700.7 (incl. ISS Addendum). NOTE 1 Pressurized hardware (including pressure vessels, pressurized structures, pressure components, and special pressurized equipment) comply with ECSS-E-ST-32-02. NOTE 2 For the attachments of pressurized hardware, which are not part of the pressurized shell, no special requirements are specified in 8.2. They follow the normal rules of this standard (e.g. be verified safe life or fail safe) to prevent catastrophic or critical hazards. |
spacebert_ecss | Solvent shall not degrade the base material or that of adjacent parts. |
spacebert_ecss | The end of the Packet containing the read-modify-write reply shall be indicated by an EOP character. |
spacebert_ecss | Approval Authority should make available the list of laboratories to perform microsection. |
spacebert_ecss | The requirements analysis method used shall be listed and referenced. NOTE Reference to applied literature or other standards can be described here. |
2005_skal1_WEB | The interface between CSP and Infra shall be compliant with the SKA- TEL.CSP.SE-TEL.INFRA.SE-ICD- 001 Interface Control Document. |
spacebert_ecss | During ignition and combustion there shall be no flaming droplets or particles. |