| S. No. |
Doc. NO. | Document Title | Stage |
|---|---|---|---|
| 1 | TED/14/19835 | Aircraft — Fuel Nozzle Grounding Plugs and Sockets — Specification | Under Published |
| 2 | TED/14/19890 | Aircraft Sealing Wire — Specification | Under Published |
| 3 | TED/14/19950 | Directions of Operation of Toggle Switches on Aircraft | Under Published |
| 4 | TED/14/19955 | Aircraft Pressure Refuelling Connection — Dimensions | Under Published |
| 5 | TED/14/20470 | Aerospace — Nuts, hexagonal, plain, normal height, normal across flats, with MJ threads, classifications: 600 MPa (at ambient temperature)/120 degrees C, 600 MPa (at ambient temperature)/235 degrees C, 900 MPa (at ambient temperature)/425 degrees C, 1 100 MPa (at ambient temperature)/235 degrees C, 1 100 MPa (at ambient temperature)/315 degrees C, 1 100 MPa (at ambient temperature)/650 degrees C, 1 210 MPa (at ambient temperature)/730 degrees C, 1 250 MPa (at ambient temperature)/235 degrees C and 1 550 MPa (at ambient temperature)/600 degrees C - Dimensions | Under Published |
| 6 | TED/14/20489 | Aerospace — Nuts, Hexagonal, Self-locking, with MJ Threads, Classifications 1 100 MPa (at Ambient Temperature)/235 °C, 1 100 MPa (at Ambient Temperature)/315 °C and 1 100 MPa (at Ambient Temperature)/ 425 °C — Dimensions | Under Published |
| 7 | TED/14/20706 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 1 GENERAL | WC-Draft |
| 8 | TED/14/20708 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 2 MOTION OF AIRCRAFT | WC-Draft |
| 9 | TED/14/20723 | Aerospace — Lead and Runout Threads Part 1 Rolled External Threads | Under Published |
| 10 | TED/14/20757 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 3 STRUCTURE | WC-Draft |
| 11 | TED/14/20759 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 4 AERODYNAMICS | WC-Draft |
| 12 | TED/14/20760 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 5 AERODYNES HEAVIER-THAN-AIR AIRCRAFT | WC-Draft |
| 13 | TED/14/20763 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 6 SPACE TERMS | WC-Draft |
| 14 | TED/14/20768 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 8 POWER PLANT | WC-Draft |
| 15 | TED/14/21135 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 7 AIR TRAFFIC AND GROUND SERVICES | WC-Draft |
| 16 | TED/14/21157 | AIR CARGO — CERTIFIED LOWER DECK CONTAINERS — DESIGN AND TESTING | WC-Draft |
| 17 | TED/14/21266 | Aerospace — Lead and Runout Threads Part 2 Internal Threads | Under Published |
| 18 | TED/14/21269 | Aerospace — Bolts, Normal Bihexagonal Head, Normal Shank, Short or Medium Length MJ Threads, Metallic Material, Coated or Uncoated, Strength Classes Less Than or Equal To 1 100 MPA – Dimensions | Under Published |
| 19 | TED/14/21271 | Aerospace — Nuts, metric — Tolerances of form and Position | Under Published |
| 20 | TED/14/21274 | Aerospace — Screws, 100 Degrees Normal Countersunk Head, Internal Offset Cruciform Ribbed or Unribbed Drive, Normal Shank, Short or Medium Length MJ Threads, Metallic Material, Coated or Uncoated, Strength Classes Less Than or Equal to 1 100 Mpa — Dimensions | Under Published |
| 21 | TED/14/21356 | AIRCRAFT GROUND EQUIPMENT — GRAPHICAL SYMBOLS | WC-Draft |
| 22 | TED/14/21429 | AIRCRAFT INNER TUBE AND TUBELESS TYRE VALVES — CORES AND CAPS — TEST METHODS | WC-Draft |
| 23 | TED/14/21434 | AIRCRAFT — ELECTRICAL CABLES — IDENTIFICATION MARKING | WC-Draft |
| 24 | TED/14/21437 | AEROSPACE — NUTS, HEXAGONAL, SLOTTED (CASTELLATED), NORMAL HEIGHT, NORMAL ACROSS FLATS, WITH MJ THREADS, CLASSIFICATIONS: 600 MPA (AT AMBIENT TEMPERATURE)/120 DEGREES C, 600 MPA (AT AMBIENT TEMPERATURE)/235 DEGREES C, 900 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C, 1 100 MPA (AT AMBIENT TEMPERATURE)/235 DEGREES C, 1 100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES C, 1 100 MPA (AT AMBIENT TEMPERATURE)/650 DEGREES C, 1 210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREES C, 1 250 MPA (AT AMBIENT TEMPERATURE)/235 DEGREES C AND 1 550 MPA (AT AMBIENT TEMPERATURE)/600 DEGREES C — DIMENSIONS | WC-Draft |
| 25 | TED/14/21439 | AIR CARGO EQUIPMENT — HANDLING SYSTEMS FOR UNIT LOAD DEVICES (ULDS) — SYMBOLS FOR PICTORIAL REPRESENTATION | WC-Draft |
| 26 | TED/14/21442 | AIRCRAFT — ELECTRICAL CONNECTORS — DESIGN REQUIREMENTS | WC-Draft |
| 27 | TED/14/21443 | Methods Of Test For Air - Land Cargo Pallet Nets | WC-Draft |
| 28 | TED/14/21448 | AIRCRAFT — JACKING PADS | WC-Draft |
| 29 | TED/14/22357 | SPACE SYSTEMS PROBABILISTIC RISK ASSESSMENT PRA | WC-Draft |
| 30 | TED/14/22361 | SPACE SYSTEMS PROGRAMME MANAGEMENT PART 1: STRUCTURING OF A PROJECT | WC-Draft |
| 31 | TED/14/22362 | SPACE SYSTEMS QUALIFICATION ASSESSMENT | WC-Draft |
| 32 | TED/14/22363 | SPACE SYSTEMS INTEGRATED LOGISTIC SUPPORT | WC-Draft |
| 33 | TED/14/22364 | SPACE SYSTEMS EXPERIENCE GAINED IN SPACE PROJECTS LESSONS LEARNED PRINCIPLES AND GUIDELINES | WC-Draft |
| 34 | TED/14/22365 | SPACE SYSTEMS RISK MANAGEMENT | WC-Draft |
| 35 | TED/14/22366 | SPACE SYSTEMS PROJECT REVIEWS | WC-Draft |
| 36 | TED/14/22367 | SPACE SYSTEMS GUIDELINES TO DEFINE THE MANAGEMENT FRAMEWORK FOR A SPACE PROJECT | WC-Draft |
| 37 | TED/14/22915 | SPACE SYSTEMS EARLY OPERATIONS PART 1 SPACECRAFT INITIALIZATION AND COMMISSIONING | WC-Draft |
| 38 | TED/14/22916 | SPACE SYSTEMS EARLY OPERATIONS PART 2 INITIALIZATION PLAN | WC-Draft |
| 39 | TED/14/22917 | SPACE SYSTEMS EARLY OPERATIONS PART 3 COMMISSIONING REPORT | WC-Draft |
| 40 | TED/14/22918 | Space systems — Structural components and assemblies | WC-Draft |
| 41 | TED/14/22920 | SPACE SYSTEMS - SUBSYSTEMSUNITS TO SPACECRAFT INTERFACE CONTROL DOCUMENT | WC-Draft |
| 42 | TED/14/22921 | SPACE SYSTEMS BELLOWS DESIGN AND OPERATION | WC-Draft |
| 43 | TED/14/22922 | SPACE SYSTEMS - SPACE ENVIRONMENT (NATURAL AND ARTIFICIAL) - OBSERVED PROTON FLUENCES OVER LONG DURATION AT GEO AND GUIDELINES FOR SELECTION OF CONFIDENCE LEVEL IN STATISTICAL MODEL OF SOLAR PROTON FLUENCES | WC-Draft |
| 44 | TED/14/22923 | SPACE ENVIRONMENT NATURAL AND ARTIFICIAL EARTHS ATMOSPHERE FROM GROUND LEVEL UPWARD | WC-Draft |
| 45 | TED/14/22924 | SPACE SYSTEMS - ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS | WC-Draft |
| 46 | TED/14/22925 | SPACE SYSTEMS LAUNCH-VEHICLE-TO-SPACECRAFT INTERFACES | WC-Draft |
| 47 | TED/14/22926 | SPACE SYSTEMS UNMANNED SPACECRAFT OPERABILITY | WC-Draft |
| 48 | TED/14/22927 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 1: VOCABULARY | WC-Draft |
| 49 | TED/14/22930 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 2 : CLEANLINESS LEVELS | WC-Draft |
| 50 | TED/14/22931 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 3 : ANALYTICAL PROCEDURES FOR THE DETERMINATION OF NON VOLATILE RESIDUES AND PARTICULATE CONTAMINATION | WC-Draft |
| 51 | TED/14/22932 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 4 : ROUGH-CLEANING PROCESSES | WC-Draft |
| 52 | TED/14/22933 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 5 : DRYING PROCESSES | WC-Draft |
| 53 | TED/14/22934 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 6 : PRECISION-CLEANING PROCESSES | WC-Draft |
| 54 | TED/14/22935 | SPACE SYSTEMS STRUCTURAL DESIGN DETERMINATION OF LOADING LEVELS FOR STATIC QUALIFICATION TESTING OF LAUNCH VEHICLES | WC-Draft |
| 55 | TED/14/22936 | SPACE SYSTEMS - CONTAMINATION AND CLEANLINESS CONTROL | WC-Draft |
| 56 | TED/14/22937 | SPACE SYSTEMS LAUNCH-VEHICLE-TO-SPACECRAFT FLIGHT ENVIRONMENTS TELEMETRY DATA PROCESSING | WC-Draft |
| 57 | TED/14/22938 | SPACE SYSTEMS SPACECRAFT-TO-LAUNCH-VEHICLE INTERFACE CONTROL DOCUMENT | WC-Draft |
| 58 | TED/14/22939 | SPACE SYSTEMS - GENERAL TEST METHODS FOR SPACECRAFT , SUBSYSTEMS AND UNITS | WC-Draft |
| 59 | TED/14/22940 | SPACE SYSTEMS - ASSESSMENT OF SURVIVABILITY OF UNMANNED SPACECRAFT AGAINST SPACE DEBRIS AND METEOROID IMPACTS TO ENSURE SUCCESSFUL POST-MISSION DISPOSAL | WC-Draft |
| 60 | TED/14/22941 | SPACE SYSTEMS - AVOIDING COLLISIONS AMONG ORBITING OBJECTS | WC-Draft |
| 61 | TED/14/22942 | SPACE SYSTEMS — LAUNCH PAD AND INTEGRATION SITE — FACILITY, SYSTEM AND EQUIPMENT FAILURE ANALYSIS | WC-Draft |
| 62 | TED/14/22943 | SPACE ENVIRONMENT (NATURAL AND ARTIFICIAL) — THE EARTH'S IONOSPHERE MODEL — INTERNATIONAL REFERENCE IONOSPHERE (IRI) MODEL AND EXTENSIONS TO THE PLASMASPHERE | WC-Draft |
| 63 | TED/14/22945 | SPACE SYSTEMS - RELATIVE MOTION ANALYSIS ELEMENTS AFTER LV/SC SEPARATION | WC-Draft |
| 64 | TED/14/22946 | SPACE SYSTEMS — The measured parameters at firing bench and flight tests of liquid rocket engines | WC-Draft |
| 65 | TED/14/22947 | SPACE SYSTEMS SIMULATION REQUIREMENTS FOR CONTROL SYSTEM | WC-Draft |
| 66 | TED/14/22948 | Space systems — Spacecraft interface requirements document for launch vehicle services | WC-Draft |
| 67 | TED/14/22949 | SPACE SYSTEMS LIQUID ROCKET ENGINES AND TEST STANDS TERMS AND DEFINITIONS | WC-Draft |
| 68 | TED/14/22950 | SPACE SYSTEMS — LITHIUM ION BATTERY FOR SPACE VEHICLES — DESIGN AND VERIFICATION REQUIREMENTS | WC-Draft |
| 69 | TED/14/22951 | SPACE SYSTEMS - INTERFACE CONTROL DOCUMENTS BETWEEN GROUND SYSTEMS GROUND SUPPORT EQUIPMENT AND LAUNCH VEHICLE WITH PAYLOAD | WC-Draft |
| 70 | TED/14/22953 | SPACE ENVIRONMENT (NATURAL AND ARTIFICIAL) — MODEL OF HIGH ENERGY RADIATION AT LOW ALTITUDES (300 KM TO 600 KM) | WC-Draft |
| 71 | TED/14/22955 | SPACE SYSTEMS — CUBE SATELLITES (CUBESATS) | WC-Draft |
| 72 | TED/14/22959 | SPACE SYSTEMS - GUIDELINES FOR THE MANAGEMENT OF SYSTEMS ENGINEERING | WC-Draft |
| 73 | TED/14/22961 | SPACE SYSTEMS — DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS | WC-Draft |
| 74 | TED/14/22963 | SPACE SYSTEMS — PRODUCT ASSURANCE REQUIREMENTS FOR COMMERCIAL SATELLITES | WC-Draft |
| 75 | TED/14/22967 | SPACE SYSTEMS REQUIREMENTS FOR SMALL SPACECRAFT | WC-Draft |
| 76 | TED/14/22971 | SPACE SYSTEMS - MASS PROPERTIES CONTROL | WC-Draft |
| 77 | TED/14/22973 | SPACE SYSTEMS - GENERAL TEST REQUIREMENTS FOR LAUNCH VEHICLES | WC-Draft |
| 78 | TED/14/22975 | SPACE SYSTEMS — SPACE LAUNCH COMPLEXES, INTEGRATION SITES AND OTHER FACILITIES — GENERAL TESTING GUIDELINES | WC-Draft |
| 79 | TED/14/22976 | SPACE SYSTEMS - ORBIT DETERMINATION AND ESTIMATION - PROCESS FOR DESCRIBING TECHNIQUES | WC-Draft |
| 80 | TED/14/22977 | SPACE SYSTEMS - CAPABILITY-BASED SAFETY DEPENDABILITY AND QUALITY ASSURANCE (SD & QA) PROGRAMME MANAGEMENT | WC-Draft |
| 81 | TED/14/22978 | SPACE SYSTEMS STRUCTURAL DESIGN LOADS AND INDUCED ENVIRONMENT | WC-Draft |
| 82 | TED/14/22979 | SPACE SYSTEMS PRESSURE VESSELS AND PRESSURIZED STRUCTURES DESIGN AND OPERATION | WC-Draft |
| 83 | TED/14/24556 | GENERAL PURPOSE PUSH-PULL SINGLE-POLE CIRCUIT-BREAKERS FOR AIRCRAFT PERFORMANCE REQUIREMENTS | WC-Draft |
| 84 | TED/14/24557 | Aircraft Electrical Connectors Tests | WC-Draft |
| 85 | TED/14/24558 | Aircraft Methodology of Calculating Cargo Compartment Volumes | WC-Draft |
| 86 | TED/14/24559 | Air Cargo Equipment Ground Equipment Requirements For Compatibility with Aircraft Unit Load Devices | WC-Draft |
| 87 | TED/14/24656 | Space Systems — Programme Management — Breakdown of Project Management Structures | WC-Draft |