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XPAA

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... RF functional tests using hat coupler, near-field scanner and anechoic chamber. ... characteristics and pointing performance, does not require an anechoic chamber. ... – PowerPoint PPT presentation

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Title: XPAA


1
Section 23 X-Band Phased Array Antenna
. . . Kenneth Perko EO-1 XPAA Lead, Microwave
Systems Branch
2
X-Band Phased Array Antenna (XPAA)
  • Validates electronically scanned antenna
    technology for future missions.
  • No moving parts, redundant SSPAs, simplified IT.
  • Designed and built by Boeing for NMP
    Communications IPDT under fixed price contract
    with GSFC.
  • Boeing assumed cost risk for deliverable item.
  • Provides 105 Mbps QPSK primary science downlink.

3
XPAA Performance Summary
  • Frequency - 8225 MHz
  • Bandwidth - 400 MHz
  • Scan Coverage - 60 deg half-angle cone
  • Radiating Elements - 64
  • RF Input - 14 dBm
  • EIRP - greater than 22 dBW at all commanded
    angles
  • Polarization - LHCP
  • Command Interface / Controller - 1773 / RSN
  • Input DC Power - lt58 watts over 0 to 40 C
  • Mass - 5.5 kg

4
EO1 X-Band Subsystem Diagram
Pointing Commands from Spacecraft via 1773
interface
XPAA
2 dB Attenuator
ESN Control Interface / Processor
Phase Settings
Science Data
Exciter/ Modulator
x 64
WARP
Coax Cables X-band Signal Modulated with Data
X-band Signal Radiated to Ground
5
XPAA Acquisition / Review Process
  • Contract Negotiations -- Continuous QA
    involvement to ensure satisfactory quality
    controls given the tight, fixed budget.
  • Technology Verifications -- Independent
    evaluation of RF modules, their packaging, and
    array communications performance by GRC on Boeing
    EM hardware. EM was environmentally tested by
    Boeing at their cost prior to PKR.
  • Formal Contract Reviews -- Program Kickoff Review
    (PKR), Interim Design Review (IDR), Antenna
    Acceptance Review (AAR). Weekly telcons.
  • Post Delivery Test -- Approach developed with
    expertise from Swales and NSI, Inc.

6
XPAA Principal Team Members
  • Name Role Relevant Experience
  • Ken Perko (567) XPAA Lead NMP Comm. IPDT
  • Fernando Pellerano (567) Requirements Ka-Phased
    Array Procurement
  • Don McMeen (Boeing) Program Mgt. Mil. Array
    Developments
  • Ray Huggins (Boeing) Array Design GRC/Mil. Array
    Developments
  • Richard Kunath (GRC) Array Testing ACTS Array
    Developments
  • Kurt Shalkhauser (GRC) RF Module Packaging ACTS
    Array Developments
  • Tom Dod (Swales) Near Field Tests GSFC Antenna
    Group
  • Alan Newell (NSI, Inc) NF EIRP Developed NF
    Tech. At NIST Measurements

7
XPAA -- Scope of Box-Level Testing
  • Contract Acceptance Testing
  • Random vibration, shock, thermal vacuum, EMI/EMC,
    1773, and RF functional tests using hat coupler,
    near-field scanner and anechoic chamber.
    Environmental levels determined by Swales
    document "Verification Plan and Specification for
    NMP Earth Orbiter 1 (EO-1)".
  • Bench Testing
  • RF and 1773 functional tests using a hat coupler
    to absorb and sample the RF output. Results
    compared with contractor supplied acceptance
    data.
  • Near-Field Scanning
  • Verifies antenna beam characteristics and
    pointing performance, does not require an
    anechoic chamber. Results compared with
    contractor supplied acceptance data.

8
XPAA Qualification Test Flow (1998)
9
XPAA Test Flow (2)
10
XPAA Trended Parameters
11
NF Scanner in Position in Front of the XPAA
During Near Field Test 3
12
Processed NF3 Data for XPAA (Theta0, Phi0)
Aperture Amplitude Far Field Cut Aperture
Phase Far Field Contour
13
XPAA Hardware Changes Since Delivery
  • Change
  • Replaced 1773 interface connector (1 of 4).
  • Reason
  • During pre-integration inspection and test this
    connector was found to have a cracked internal
    ceramic sleeve.
  • Action
  • RSN card was removed and connector was replaced
    at GSFC FOIL.
  • Result of the Modification
  • After repair and workmanship vibration,
    end-to-end 1773 and RF performance was verified
    with GSE and Near-Field Scanner at Swales.

14
XPAA Software Changes Since Delivery
  • Change
  • Updated RSN operating system.
  • Reason
  • EO-1 requires all RSNs use the same operating
    system version.
  • Change
  • Box-level fault detection constants updated.
    (Addressed PRs on next slide.)
  • Reason
  • Prevent false alarms.
  • Change
  • Telemetry A/D time constants changed (all RSNs)
    after NF3.
  • Reason
  • EO-1 requires all RSNs use the same operating
    system version.

15
XPAA Critical PRs
16
XPAA Action Item Status
  • No open items.
  • XPAA on-time since integration as recorded by
    EO-1 -- gt350 hours, Data Collection Events
    (downlinks) gt300.

17
XPAA Statement of Readiness
  • The XPAA is ready to fly.
  • There are no known Redbook issues.
  • No special tests for the XPAA (such as pointing)
    are planned beyond normal IT activities.
  • There is one issue of low residual risk
  • Software change after last NF test, to an A-to-D
    wait-state constant, required for all RSNs.
  • This affects analog measurements (telemetry) on
    the RSN.
  • Does not affect the XPAA beam-pointing code at
    all.
  • Telemetry will be re-evaluated during IT.
  • Software is repairable in-flight using a patch to
    RAM.
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