SATPC0033519 Tab 04 SOW.pdf
PDF 134 KB Posted
- Attached to
- AC/DC Power Converter (Regulated Power Conversion Unit - RPCU) Federal contract opportunity
- Solicitation number
- 80NSSC24853768Q-1
About this file
This statement of work outlines requirements for an AC/DC power converter for a NASA aircraft modification project. The Airborne Science Program is modifying a G-IV aircraft and requires a power converter with the following specifications: an input of 115VAC, 324-800Hz, 3-phase; regulated 28VDC, 0.250A continuous output; power quality meeting MIL-STD-704F; EMI/EMC meeting MIL-STD-461G; full performance from -55C to +70C; qualification to RTCA/DO-160G and RTCA/DO-254 with a DAL B; weighing 17.5 lbs and measuring 7.50 in x 12.82 in x 5.1 in. The statement of work requests three units with delivery expected within 26 weeks to the NASA Armstrong Flight Research Center. The related federal contract opportunity is solicitation number 80NSSC24853768Q-1 from NASA Shared Services Center for the AC/DC power converter.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SATPC0033519 Tab 10 RFQ Full and Open.pdf |
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Text version
STATEMENT OF WORK
1. Objective/Requirements The AirSAR-NG project is modifying a G-IV aircraft for the Airborne Science Program. To complete the mission system modifications the project requires the use of an AC/DC Power Converter. This is for the procurement of that power converter.
2. Characteristics, Scope, and Specs
The specifications are as follows:
• Power Input: 115VAC, 324–800Hz, 3-phase
• Power Output: Regulated 28VDC ±0.3VDC, 250 Amps continuous
• Power Quality: MIL-STD-704F
• EMI/EMC: MIL-STD-461G
• Full performance from: -55°C to +70°C
• Qualification: RTCA/DO-160G; RTCA/DO-254 DAL B
• Weight: 17.5 lbs (7.94 kg)
• Size: 7.50 in W x 12.82 in L x 5.1 in H
3. Quantity: Three (3)
4. Place of Performance
Delivery to NASA Armstrong Flight Research Center.
5. Period of Performance Delivery is expected within 26 weeks or less ARO.
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