| Standard No. |
Title |
Price(USD) |
Delivery |
Status |
Add To Cart |
| QJ 2655.2-1994 |
Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Temperature |
90 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 1275-1994 |
Assessment on Measurement Uncertainty of Solid Rocket Motor |
480 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2655.4-1994 |
Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Fuel Flow |
90 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2655.5-1994 |
Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Air Flow |
90 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2655.3-1994 |
Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Thrust |
90 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2654-1994 |
Test Specification for Liquid Rocket Engine (LRE) Thrust Chamber |
255 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2655.6-1994 |
Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Rotational Speed |
75 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2613-1994 |
Whirling Test Method for Solid Rocket Motor |
435 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2612-1994 |
General Technical Specifications for Fuel Regulator of Liquid Ramjet in Air-Hydraulic Type |
135 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2609-1994 |
High-energy X-ray Flaw Detection Method for Combustion Chamber in Solid Rocket Motor |
150 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 2610-1994 |
Test Method for Nozzle Deflection Angle of Solid Rocket Motor |
150 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ A 1488-2004 |
QJ A 1488-2004 General Specification for Chamber Insulation Liner and Stress Release Boot of Solid Rocket Motor |
240 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 1003A-2004 |
|
135 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ A 2748-2004 |
QJ A 2748-2004 General Technical Requirements for Seal Structure of Solid Rocket Motor |
150 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ A 1004-2004 |
QJ A 1004-2004 Stable Test Procedure of Solid Rocket Motor |
120 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 3197-2004 |
Non-destructive Inspection Method for Filament-wound Combustor Case of Solid Rocket Motor |
|
via email in
1 business day
|
VALID
|
please email coc@codeofchina.com for quotation
|
| QJ A 1003-2004 |
QJ A 1003-2004 Design Procedure for Liquid Propellant Rocket Engine |
120 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ A 2038.1-2004 |
QJ A 2038.1-2004 Test Method for Interface Bonding Strength of Solid Rocket Motor Chamber - Part 1: Unstick Test for Rectangular Specimen |
150 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 3159.1-2002 |
Method of Test Data Processing for Missile Used Turbojet - Part1: Stand Bed Test |
270 (USD) |
via email in
1 business day
|
VALID
|
|
| QJ 3144-2002 |
Determination for Hazard Classification and Safe Distance of Composite Solid Propellant Workshop Building |
375 (USD) |
via email in
1 business day
|
VALID
|
|
|
|
