Follow this link to go to the text only version of nasa.gov
NASA - National Aeronautics and Space Administration
Follow this link to skip to the main content
+ Low Bandwidth
+ Contact NASA
Go
Top Spacer

Environmental Test Engineering and Integration
Code 549
Environmental Project
Structural Dynamics
Electromagnetic
Space Simulation
Facilities
- T/V Facility 225 (9'x14')
- T/V Facility 237 (7' x 8')
- T/V Facility 238 (12' x 14')
- T/V Facility 239 (7' x 8')
- T/V Facility 240 (3' x 3')
- T/V Facility 241 (3' x 4')
- T/V Facility 245 (2' x 3')
- T/V Facility 246 (3.5' x 5.5')
- T/V Facility 281 (3' x 4')
- T/V Facility 290 (27' x 40')
- T/H Facility 204 (2.2 ft³)
- T/H Facility 232 (64 ft³)
- T/H Facility 233 (64 ft³)
Personnel
 
Facility 225 is a large, horizontal, cylindrical, thermal vacuum chamber used for thermal vacuum and thermal balance testing, and baking out large test items. Electrical feedthroughs and liquid and gas penetrations are provided at locations on the front, sides, and rear of the chamber.
Facility 225

Mode of Operation

Test items are loaded by crane onto a load cart, which is rolled into the chamber on a rail system. Payload weight can be as high as 5,000 lb. The chamber door remains open while thermocouples are installed on the test item inside the chamber. A temperature controlled baseplate may be provided for high thermal dissipation.

Chamber evacuation is provided by 2 cryopumps, while roughing is provided by a blower and rotary vane machanical pump. Shroud temperature condidtioning is accomplished by a recirculating GN2 thermal system, or it may be flooded with LN2.


Parameters


Test Pressure: 1 x 10-7 mmHg
Shroud Temperature:
GN2 mode -140°C to +100°C , LN2 mode -190°C
Chamber Pump: 2 cryopumps


Physical Characteristics

Test Volume: 9' x 14'
Payload Support: Wheeled cart - 5,000 lb. capacity
Std. electrical feedthroughs: 61-pin, 37-pin, 7-pin, 4-pin, RF

Integral Instrumentation


Pressure: Capacitance manometer - Atm to 10-3 mmHg
Ion Gauge: 10-3 mmHg to ultimate
Payload Temperature: 320 thermocouple channels
Contamination Monitor: TQCM, coldfinger, residual gas analyzer

 



NASA Goddard Space Flight Center
FirstGov - Your First Click to the US Government
+ Freedom of Information Act
+ Budgets, Strategic Plans and Accountability Reports
+ The President's Management Agenda
+ NASA Privacy Statement, Disclaimer,
and Accessibility Certification

+ Inspector General Hotline
+ Equal Employment Opportunity Data Posted Pursuant
to the No Fear Act

+ Information-Dissemination Priorities and Inventories
NASA - National Aeronautics and Space Administration
Editor: J. Killam
NASA Official: D. Robinson
Last Updated: March 25, 2024
+ Contact NASA