Document Details |
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| Name of Department/Committee : | TED 14 |
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| Document Number : | TED 14 ( 22946) |
| Document Title [English] : | SPACE SYSTEMS — The measured parameters at firing bench and flight tests of liquid rocket engines |
| Document Title [Hindi] : | अंतरिक्ष प्रणालियां — तरल रॉकेट इंजनों की फायरिंग बेंच और उड़ान परीक्षणों में मापे गए पैरामीटर |
| Document Type : | New |
| Language : | English |
| Priority : | 1 |
| ICS Code : | 49.140 |
| Date of Project Approval : | 06-07-2023 |
| Standards to be Superseded : | |
Classification Details |
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| Group : | Transport and Logistics Services |
| Sub Group : | Transport and Logistics Services |
| Sub Sub Group : | Transport Services |
| Aspects : | Process Specification |
| Risk : | Low |
| Certification : | None |
| Short Commom Man's Title : | |
| ITCHS Code : | |
| Ministry : |
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| Sustainable development Goals : |
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| Degree of Equivalence : | Identical under dual numbering |
| Identical/Equivalent Standards : | ISO 16694 : 2015 |
| Organization Type: | ISO |
| Sl.No. | Synosis Points | |
| 1 | This standard is identical adoption of ISO 16694:2015. | |
| 2 | This International Standard applies to all types of liquid rocket engines for expendable launch systems and satellites: a. Combustible fuel (including cryogenic); b. Large-thrust, multiple component engines, with and without afterburning; c. Low-thrust engines, one component (mono-propellant) and two-component (bi-propellant). | |
| 3 | This International Standard establishes a list of parameters to be measured and registered with the firing stand and flight tests of serial LRE. The order of preparation and carrying out of stand and flight tests, methods of processing, and analysis of tests results of liquid rocket engines, also measurement accuracy requirements are not regulated by this International Standard. Measurement accuracy requirements are established by engine designer. Parameters listed in this International Standard characterize performance attributes of liquid rocket engines and are used for evaluating of technical state of engines (operative, inoperative), if they correspond to the requirements specified and possibilities of putting them into operation. There are parameters specified in this International Standard, obligatory for registration and optional ones. The manufacturer of liquid rocket engines can determine additional list of parameters for specific items taking into account their design and | |
Timeline Details |
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Stages |
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| Sl. No. |
Stage | Date of Occurence | Remarks | Circulated to | Files |
| 1 | Generation of Document Number | 06-07-2023 | ------- | ||
| 2 | P-Draft Waived | 28-07-2023 | During 27th SC meeting, the committee decided to WC the document for 60 days. | ------- | |
| 3 | WC Draft | 28-07-2023 | Duration : 60 Days Submitted for HOD approval |
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| 4 | WC Draft | 28-07-2023 | WC rejected by HOD Remarks: Please check the Title of the document |
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| 5 | WC Draft | 31-07-2023 | Duration : 60 Days Submitted for HOD approval |
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| 6 | WC Draft | 31-07-2023 | WC approved by HOD |
TEDC | ------- |
| 7 | WC Draft | 29-07-2024 | Duration : 30 Days Submitted for HOD approval Remarks : The document is being wide circulated for 30 days for comments |
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| 8 | WC Draft | 30-07-2024 | WC approved by HOD |
TEDC | ------- |