History
Document Details
Name of Department/Committee : TED 14
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Standards to be Superseded :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
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 :
  • Ministry of Civil Aviation
Sustainable development Goals :
  • INDUSTRY, INNOVATION AND INFRASTRUCTURE
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


S.No. P-Draft
Completion Date		 WC-Draft
Completion Date		 Final-Draft
Completion Date		 Project
Completion Date(Gazette)		 Entered By Entered On
1 14-07-2023 14-10-2023 14-11-2023 14-01-2024 SHRI SHIVAM AGGARWAL 14-07-2023
Stages
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 		-------
4 WC Draft 28-07-2023 WC rejected by HOD
Remarks: Please check the Title of the document 		-------
5 WC Draft 31-07-2023 Duration : 60 Days
Submitted for HOD approval 		-------
6 WC Draft 31-07-2023 WC approved by HOD
 TEDC   -------