S. No. |
Doc. NO. | Document Title | Stage |
---|---|---|---|
1 | 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 |
2 | TED/14/20706 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 1 GENERAL | WC-Draft |
3 | TED/14/20708 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 2 MOTION OF AIRCRAFT | WC-Draft |
4 | TED/14/20757 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 3 STRUCTURE | WC-Draft |
5 | TED/14/20759 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 4 AERODYNAMICS | WC-Draft |
6 | TED/14/20760 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 5 AERODYNES HEAVIER-THAN-AIR AIRCRAFT | WC-Draft |
7 | TED/14/20763 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 6 SPACE TERMS | WC-Draft |
8 | TED/14/20768 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 8 POWER PLANT | WC-Draft |
9 | TED/14/21135 | GLOSSARY OF AERONAUTICAL AND ASTRONAUTICAL TERMS PART 7 AIR TRAFFIC AND GROUND SERVICES | WC-Draft |
10 | TED/14/21157 | AIR CARGO — CERTIFIED LOWER DECK CONTAINERS — DESIGN AND TESTING | WC-Draft |
11 | TED/14/21356 | AIRCRAFT GROUND EQUIPMENT — GRAPHICAL SYMBOLS | WC-Draft |
12 | TED/14/21429 | AIRCRAFT INNER TUBE AND TUBELESS TYRE VALVES — CORES AND CAPS — TEST METHODS | PDF Sent To Technical Department |
13 | TED/14/21434 | AIRCRAFT — ELECTRICAL CABLES — IDENTIFICATION MARKING | WC-Draft |
14 | 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 |
15 | TED/14/21439 | AIR CARGO EQUIPMENT — HANDLING SYSTEMS FOR UNIT LOAD DEVICES (ULDS) — SYMBOLS FOR PICTORIAL REPRESENTATION | WC-Draft |
16 | TED/14/21442 | AIRCRAFT — ELECTRICAL CONNECTORS — DESIGN REQUIREMENTS | WC-Draft |
17 | TED/14/21443 | Methods Of Test For Air - Land Cargo Pallet Nets | WC-Draft |
18 | TED/14/21448 | AIRCRAFT — JACKING PADS | WC-Draft |
19 | TED/14/22357 | SPACE SYSTEMS PROBABILISTIC RISK ASSESSMENT PRA | Under Published |
20 | TED/14/22361 | SPACE SYSTEMS PROGRAMME MANAGEMENT PART 1: STRUCTURING OF A PROJECT | Under Published |
21 | TED/14/22362 | SPACE SYSTEMS QUALIFICATION ASSESSMENT | WC-Draft |
22 | TED/14/22363 | SPACE SYSTEMS INTEGRATED LOGISTIC SUPPORT | WC-Draft |
23 | TED/14/22364 | SPACE SYSTEMS EXPERIENCE GAINED IN SPACE PROJECTS LESSONS LEARNED PRINCIPLES AND GUIDELINES | WC-Draft |
24 | TED/14/22365 | SPACE SYSTEMS RISK MANAGEMENT | WC-Draft |
25 | TED/14/22366 | SPACE SYSTEMS PROJECT REVIEWS | WC-Draft |
26 | TED/14/22367 | SPACE SYSTEMS GUIDELINES TO DEFINE THE MANAGEMENT FRAMEWORK FOR A SPACE PROJECT | WC-Draft |
27 | TED/14/22915 | SPACE SYSTEMS EARLY OPERATIONS PART 1 SPACECRAFT INITIALIZATION AND COMMISSIONING | WC-Draft |
28 | TED/14/22916 | SPACE SYSTEMS EARLY OPERATIONS PART 2 INITIALIZATION PLAN | WC-Draft |
29 | TED/14/22917 | SPACE SYSTEMS EARLY OPERATIONS PART 3 COMMISSIONING REPORT | WC-Draft |
30 | TED/14/22918 | Space systems — Structural components and assemblies | Under Published |
31 | TED/14/22920 | SPACE SYSTEMS - SUBSYSTEMSUNITS TO SPACECRAFT INTERFACE CONTROL DOCUMENT | F-Draft |
32 | TED/14/22921 | SPACE SYSTEMS BELLOWS DESIGN AND OPERATION | WC-Draft |
33 | 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 |
34 | TED/14/22923 | SPACE ENVIRONMENT NATURAL AND ARTIFICIAL EARTHS ATMOSPHERE FROM GROUND LEVEL UPWARD | WC-Draft |
35 | TED/14/22924 | SPACE SYSTEMS - ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS | WC-Draft |
36 | TED/14/22925 | SPACE SYSTEMS LAUNCH-VEHICLE-TO-SPACECRAFT INTERFACES | F-Draft |
37 | TED/14/22926 | SPACE SYSTEMS UNMANNED SPACECRAFT OPERABILITY | Under Published |
38 | TED/14/22927 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 1: VOCABULARY | WC-Draft |
39 | TED/14/22930 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 2 : CLEANLINESS LEVELS | WC-Draft |
40 | 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 |
41 | TED/14/22932 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 4 : ROUGH-CLEANING PROCESSES | WC-Draft |
42 | TED/14/22933 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 5 : DRYING PROCESSES | WC-Draft |
43 | TED/14/22934 | SPACE SYSTEMS - SURFACE CLEANLINESS OF FLUID SYSTEMS - PART 6 : PRECISION-CLEANING PROCESSES | WC-Draft |
44 | TED/14/22935 | SPACE SYSTEMS STRUCTURAL DESIGN DETERMINATION OF LOADING LEVELS FOR STATIC QUALIFICATION TESTING OF LAUNCH VEHICLES | WC-Draft |
45 | TED/14/22936 | SPACE SYSTEMS - CONTAMINATION AND CLEANLINESS CONTROL | WC-Draft |
46 | TED/14/22937 | SPACE SYSTEMS LAUNCH-VEHICLE-TO-SPACECRAFT FLIGHT ENVIRONMENTS TELEMETRY DATA PROCESSING | WC-Draft |
47 | TED/14/22938 | SPACE SYSTEMS SPACECRAFT-TO-LAUNCH-VEHICLE INTERFACE CONTROL DOCUMENT | WC-Draft |
48 | TED/14/22939 | SPACE SYSTEMS - GENERAL TEST METHODS FOR SPACECRAFT , SUBSYSTEMS AND UNITS | Under Published |
49 | 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 |
50 | TED/14/22941 | SPACE SYSTEMS - AVOIDING COLLISIONS AMONG ORBITING OBJECTS | WC-Draft |
51 | TED/14/22942 | SPACE SYSTEMS — LAUNCH PAD AND INTEGRATION SITE — FACILITY, SYSTEM AND EQUIPMENT FAILURE ANALYSIS | WC-Draft |
52 | 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 |
53 | TED/14/22945 | SPACE SYSTEMS - RELATIVE MOTION ANALYSIS ELEMENTS AFTER LV/SC SEPARATION | WC-Draft |
54 | TED/14/22946 | SPACE SYSTEMS — The measured parameters at firing bench and flight tests of liquid rocket engines | WC-Draft |
55 | TED/14/22947 | SPACE SYSTEMS SIMULATION REQUIREMENTS FOR CONTROL SYSTEM | Under Published |
56 | TED/14/22948 | Space systems — Spacecraft interface requirements document for launch vehicle services | Under Published |
57 | TED/14/22949 | SPACE SYSTEMS LIQUID ROCKET ENGINES AND TEST STANDS TERMS AND DEFINITIONS | WC-Draft |
58 | TED/14/22950 | SPACE SYSTEMS — LITHIUM ION BATTERY FOR SPACE VEHICLES — DESIGN AND VERIFICATION REQUIREMENTS | WC-Draft |
59 | TED/14/22951 | SPACE SYSTEMS - INTERFACE CONTROL DOCUMENTS BETWEEN GROUND SYSTEMS GROUND SUPPORT EQUIPMENT AND LAUNCH VEHICLE WITH PAYLOAD | Under Published |
60 | TED/14/22953 | SPACE ENVIRONMENT (NATURAL AND ARTIFICIAL) — MODEL OF HIGH ENERGY RADIATION AT LOW ALTITUDES (300 KM TO 600 KM) | WC-Draft |
61 | TED/14/22955 | SPACE SYSTEMS — CUBE SATELLITES (CUBESATS) | Under Published |
62 | TED/14/22959 | SPACE SYSTEMS - GUIDELINES FOR THE MANAGEMENT OF SYSTEMS ENGINEERING | Under Published |
63 | TED/14/22961 | SPACE SYSTEMS — DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS | WC-Draft |
64 | TED/14/22963 | SPACE SYSTEMS — PRODUCT ASSURANCE REQUIREMENTS FOR COMMERCIAL SATELLITES | Under Published |
65 | TED/14/22967 | SPACE SYSTEMS REQUIREMENTS FOR SMALL SPACECRAFT | WC-Draft |
66 | TED/14/22971 | SPACE SYSTEMS - MASS PROPERTIES CONTROL | Under Published |
67 | TED/14/22973 | SPACE SYSTEMS - GENERAL TEST REQUIREMENTS FOR LAUNCH VEHICLES | Under Published |
68 | TED/14/22975 | SPACE SYSTEMS — SPACE LAUNCH COMPLEXES, INTEGRATION SITES AND OTHER FACILITIES — GENERAL TESTING GUIDELINES | WC-Draft |
69 | TED/14/22976 | SPACE SYSTEMS - ORBIT DETERMINATION AND ESTIMATION - PROCESS FOR DESCRIBING TECHNIQUES | WC-Draft |
70 | TED/14/22977 | SPACE SYSTEMS - CAPABILITY-BASED SAFETY DEPENDABILITY AND QUALITY ASSURANCE (SD & QA) PROGRAMME MANAGEMENT | WC-Draft |
71 | TED/14/22978 | SPACE SYSTEMS STRUCTURAL DESIGN LOADS AND INDUCED ENVIRONMENT | WC-Draft |
72 | TED/14/22979 | SPACE SYSTEMS PRESSURE VESSELS AND PRESSURIZED STRUCTURES DESIGN AND OPERATION | Under Published |
73 | TED/14/24556 | GENERAL PURPOSE PUSH-PULL SINGLE-POLE CIRCUIT-BREAKERS FOR AIRCRAFT PERFORMANCE REQUIREMENTS | WC-Draft |
74 | TED/14/24557 | Aircraft Electrical Connectors Tests | WC-Draft |
75 | TED/14/24558 | Aircraft Methodology of Calculating Cargo Compartment Volumes | WC-Draft |
76 | TED/14/24559 | Air Cargo Equipment Ground Equipment Requirements For Compatibility with Aircraft Unit Load Devices | WC-Draft |
77 | TED/14/24656 | Space Systems — Programme Management — Breakdown of Project Management Structures | WC-Draft |
78 | TED/14/26250 | AIRCRAFT-PALLET DOLLEY FUNCTIONAL REQUIREMENTS | WC-Draft |