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FBO DAILY ISSUE OF APRIL 09, 2004 FBO #0865
SOLICITATION NOTICE

A -- Deployable Structures Experiment (DSX) Host Spacecraft Bus (HSB)

Notice Date
4/7/2004
 
Notice Type
Solicitation Notice
 
NAICS
541710 — Research and Development in the Physical, Engineering, and Life Sciences
 
Contracting Office
Department of the Air Force, Air Force Materiel Command, AFRL, Space Vehicles Directorate, Kirtland AFB, 2251 Maxwell Ave, Kirtland AFB, NM, 87117
 
ZIP Code
87117
 
Solicitation Number
Reference-Number-VS-PKVI-04-01
 
Response Due
5/10/2004
 
Point of Contact
Shari Barnett, Contracting Officer, Phone (505) 846-6189, Fax (505) 846-7549, - Dave Ferguson, Contract Specialist, Phone 505 846 7601, Fax 505 846 7549,
 
E-Mail Address
shari.barnett@kirtland.af.mil, David.Ferguson@Kirtland.AF.MIL
 
Description
Deployable Structures Experiment (DSX) Host Spacecraft Bus (HSB): The DSX is a space flight experiment currently in execution by the Air Force Research Laboratory (AFRL) Space Vehicles Directorate. DSX is designed to conduct basic research experiments in 5 technical areas: 1) Large Deployable Structures, 2) System identification and adaptive control of the structural dynamics associated with large lightweight deployed structures, 3) Thin-film Photovoltaics, 4) Very Low Frequency (VLF) wave transmission and propagation in the magnetosphere, and 5) Space Weather. AFRL is requesting proposals (technical and cost) in response to this Broad Area Announcement (BAA). The objective of this BAA is the design, fabrication, environmental testing and delivery to AFRL/VS of a Host Spacecraft Bus with the capability to provide standard bus functions in support of the 5 DSX experiments. Integration of the HSB with the DSX experiments, integrated environmental testing, launch vehicle integration, and mission operations shall be performed by AFRL or designated contractor at Kirtland AFB. Innovation within the HSB development shall be directed towards lowering cost and increasing the responsiveness of both DSX and AFRL research and development (R&D) spacecraft in general. Key technologies may include standardized electrical and mechanical interfaces suitable to a range of potential experiments, designs that increase launch opportunities, and novel concepts that result in significant cost reduction. See attachments for further details.
 
Record
SN00561627-W 20040409/040407212038 (fbodaily.com)
 
Source
FedBizOpps.gov Link to This Notice
(may not be valid after Archive Date)

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