Approved Terms
Policy: CCSDS Blue Book
Authority: CCSDS.SEA
OID: 1.3.112.4.30
Contents
4140 records in registry
Object Identifier
Label
| Details | Status | Term | Definition | Technical Domain | References | OID | |
|---|---|---|---|---|---|---|---|
Provisional |
a-basis allowable |
mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.1 |
|||
Provisional |
a-basis allowable |
A-basis allowable (preferred term) mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.2 |
|||
Provisional |
a-basis allowable |
mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.3 |
|||
Provisional |
a-basis allowable |
mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.4 |
|||
Provisional |
a-basis allowable |
mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.5 |
|||
Provisional |
A-basis design allowable |
A-basis allowable (preferred term) mechanical strength value above which at least 99 % of the population of values is expected to fall, with a confidence level of 95 % |
Space Systems Design Engineering |
1.3.112.4.30.2.6 |
|||
Provisional |
abbreviated checklist |
comprehensive list of items and time schedule of tasks to be done that are needed to check each stepby-step task at the telemetry/command (TLM/CMD) console and at the network console |
Space Systems Operations |
1.3.112.4.30.2.7 |
|||
Provisional |
LV/SC separation |
event of disconnection between LV/SC under the control of LV |
Space Systems Operations |
1.3.112.4.30.2.1278 |
|||
Provisional |
ablation |
chemical change and removal of surface material (3.1.12) due to the action of external high temperature heating |
Space Systems Materials & Processes |
1.3.112.4.30.2.8 |
|||
Provisional |
ablation cooling |
prevention of engine design element overheating through heat absorption by a material with its mass entrapment |
Space Systems Interfaces, Integration and Test |
1.3.112.4.30.2.9 |
|||
Provisional |
absolute capacitance |
satellite capacitance (preferred term) capacitance between a satellite body and the ambient plasma |
Space Environments |
1.3.112.4.30.2.10 |
|||
Provisional |
absorbed dose |
amount of energy imparted by ionizing radiation per unit mass of irradiated matter |
Space Environments |
1.3.112.4.30.2.11 |
|||
Provisional |
absorbed dose |
amount of energy imparted by ionizing radiation per unit mass of irradiated matter |
Space Environments |
1.3.112.4.30.2.12 |
|||
Provisional |
absorptance |
quotient of absorbed radiant flux (3.8) and incident radiant flux, expressed by |
Space Systems Materials & Processes |
1.3.112.4.30.2.13 |
|||
Provisional |
accelerated test |
test designed to shorten the controlled environmental test time with respect to the service use time by increasing the frequency of occurrence, amplitude, duration, or any combination of these of environmental stresses during service use. [7] [7] MIL-STD-810. DEPARTMENT OF DEFENSE TEST METHOD STANDARD ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS”. |
Space Systems Design Engineering |
1.3.112.4.30.2.14 |
|||
Provisional |
acceleration factor |
ratio of dose rate between simulation and expectation at space application for the same type of radiation |
Space Environments |
1.3.112.4.30.2.15 |
|||
Provisional |
manufacturer of modernized product item |
organization that performs work on pre-production and production of the upgraded product item by working design documentation |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.1317 |
|||
Provisional |
acceptable risk |
safety (3.210) risk (3.206), the severity (3.215) and the probability of which may be reasonably accepted by humanity, without durable or irreversible foreseeable consequence on health, Earth, and the environment (3.92), at the present time and in the future |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.16 |
|||
Provisional |
acceptable risk |
safety risk, the severity, and the probability (3.1.3) of which, may be reasonably accepted by humanity, without durable or irreversible foreseeable consequences on health, Earth, and the environment, at the present time and in the future |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.17 |
|||
Provisional |
acceptable risk |
safety risk, the severity and the probability of which can be reasonably accepted by humanity, without durable or irreversible foreseeable consequence on health, Earth, and the environment, at the present time and in the future |
Space Systems Interfaces, Integration and Test |
1.3.112.4.30.2.18 |
|||
Provisional |
acceptance |
|
Space Systems Programme Management and Quality |
1.3.112.4.30.2.19 |
|||
Provisional |
acceptance criteria |
minimum requirements (3.201) that it is necessary for an item (3.134) to satisfy for formal acceptance (3.2, 3.3) |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.20 |
|||
Provisional |
acceptance load |
acceptance load load applied during acceptance testing and which is equal to the limit load multiplied by an acceptance factor Jp |
Space Systems Design Engineering |
1.3.112.4.30.2.21 |
|||
Provisional |
acceptance of risk |
decision to cope with consequences, should a risk (3.206) scenario materialize |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.22 |
|||
Provisional |
acceptance of risk |
decision to cope with consequences, should a risk scenario materialise |
Space Systems Programme Management and Quality |
1.3.112.4.30.2.23 |