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01/15/2004 TIPS/JIM
Summary of the JWST Mission and ObservatorySystems Requirements Reviews,
andMicro-Shutter Array (MSA) Confirmation Review
Jerry Kriss
01/15/2004 TIPS/JIM
SRR Objectives
Confirm that mission-level and observatory requirements meet the project objectives
Confirm observatory-level specifications are sufficient to meet the project objectives
Validate that the mission architecture concept can support the functional, operational, interface and performance requirements
Show that the requirements have been flowed down and are understood at the next level.
01/15/2004 TIPS/JIM
SRR Review Team
Dennis Dillman, Chair GSFC System Review OfficeSteve Graham GSFC Project ManagementAlain Berinstain CSATed Harper CSAJacques Louet ESAColin Jones ESASteve Scott GSFC Chief EngineerAlexander Krimchansky GSFCGene Waluschka GSFC OpticsSachi Babu GSFC DetectorsTom McCarthy GSFC ThermalMark Fontaine GSFCJoe Schepis GSFC ElectromechanicalPeiman Maghami GSFCMinh Phan GSFCDr. Mal Niedner GSFC Space Sciences
01/15/2004 TIPS/JIM
NIRCam SRD
NIRSpec SRD
MIRI SRD
FGS SRD
JWST Requirements Tree
JWST-ICD-002001 JWST-ICD-001998
JWST Program PlanJWST-PLAN-000633Program
System
JWST PerformanceAssurance Requirements
JWST-RQMT-000650
JWST ScienceRequirements Document
JWST-RQMT-002558
JWST Mission OperationsConcept DocumentJWST-OPS-002018
Segment
Performance QualityAssurance Plan
JWST-PLAN-002412
Contamination ControlPlan
JWST-PLAN-002028
JWST ObservatorySpecification
JWST-SPEC-002020
Environmental Req’sfor the JWST Observatory
JWST-SPEC-003149
EMC Control PlanJWST-PLAN-002449
WFS&C RequirementsAllocation DocumentJWST-RQMT-002017
Ground SegmentRequirements
JWST-RQMT-001056
JWST SystemVerification Plan
JWST-PLAN-002027
Launch SegmentSpecification
JWST-SPEC-001999
Flight Observatory toGround Segment IRD
JWST-IRD-000696
Observatory to LaunchSegment IRD
JWST-IRD-002000
NIRCam OCD
NIRSpec OCD
MIRI OCD
FGS OCD
Radiation RequirementsAllocation SpecificationJWST-SPEC-000871
ISIM to OTE and
JWST-ICD-001831
Fault ProtectionRequirements Document
JWST-RQMT-002450
ISIM to OTE and Spacecraft IRD
JWST-IRD-000640
OTE SpecificationJWST-RQMT-002021
SC Requirements DocumentJWST-RQMT-002039
ISIM RequirementsDocument
JWST-RQMT-000835
Element
Spacecraft to OTE ICD
D35231
L1
SR
JWST MissionRequirements
JWST-RQMT-000634MR MOC PA
GS OBS
ISIM
EVRD
WFSCCPPQ
EMC
OL
OLC
LS
FP
FG
FGC
IOS-IR
IOSC
OTESOICSC
BaselinedIn CM ReviewDrafts AvailableAllocation Documents
BudgetsWFE Rev Q 03-JWST-0405
EfficiencyPointing
D36128
Observatory to GSE IRDD36127 OG
OGC
Observatory I&T PlanJWST-PLAN-002030
01/15/2004 TIPS/JIM
JWST Science Requirements (John Mather presenting)
Four themes: • First Light • Assembly of Galaxies • Birth of Star and Planetary Systems • Planetary Systems and the Origins of Life
Level 1 Mission Success Criteria: • Density of galaxies • Spectra of galaxies • Physical and Chemical properties of young stellar objects • Observing time---5 yr mission, 1.1e9 s on target • Telescope > 25 m2 • Strehl ratio > 0.8 at 2 m • Encircled energy > 0.74 within 0.15 arc sec at 1 m, stable for > 24 hrs. • Thermal environment zodi limited 0.6 -- 10 m
Example of how Level 1 requirements flow down: 1st-light objects are rare (<1 arcmin-2) ==> large, unvignetted FOV with low distortion.
01/15/2004 TIPS/JIM
Requirement Changes Since the Delta-MDR
Redesigned sun shield---smaller, better clearances, simpler deployment – but, it could make mission planning more difficult.
Upgrade the power system to accommodate ISIM power needs.
01/15/2004 TIPS/JIM
Requirements Still in Work Moving targets. Quantitative requirements are TBD,
depending on cost. Sensitivity. New numbers developed, but CCB on hold
pending NGST replan contract change. Mass allocations are TBD pending resolution of the ISIM
Electronics Compartment (IEC) study. Ariane 5 change not yet flowed down (no expected impact). FOV offsets not yet flowed done (no expected impact). Reliability. Recent MRD change says goal is 92% for
Spacecraft+OTE. Goal for whole observatory is pending. OTE to ISIM structural interface definition. X vs. Ka-band study. [Should finish soon in favor of Ka.]
01/15/2004 TIPS/JIM
Key Issues
Concept for locating ISIM electronics in Region 2 is not viable. • FPEs must be within 6m of focal planes, in Region 2 • Adding ICE boxes advantageous
• "Saddle-bag" configuration won't work. (Too massive; thermal problems.) Further work underway. (IEC trade study. Will take FPE
rqmnts into account.) Mass Allocations
• Current mass reserves are at 21%. Would like to be at 25%. Biggest problem areas are the IEC accommodation, and the sun shield containment system.
• Spacecraft is 250 kg over its allocation• OTE is 405 kg over its allocation• MIRI dewar is 20 kg over its allocation; NIRCam is 7 kg too heavy.
01/15/2004 TIPS/JIM
(ISIM Region 1)
(ISIM Region 2)
(ISIM Region 3)
01/15/2004 TIPS/JIM
SRR Summary Results
The board thought that the review was excellent. ~60 Requests for Action (RFAs) generated. Major issues in the RFAs:
• Request for an Observatory-level TV test.
• Request for deployment tests in TV.
• Desire to make several of the Mission/Obs rqmnts less vague and more verifiable (e.g., those related to event-drive ops).
• Need to do a better flow down of the efficiency rqmnt and tie it in to data quality and reliability in a more comprehensive way.
• Fault handling requires more development.
01/15/2004 TIPS/JIM
Micro-Shutter Array (MSA) Confirmation Review
Held 12/18/03 at GSFC to assess whether the MEMS micro-shutter array should be the slit-defining mechanism for NIRSpec.
Successes:• Fabricated 128 x 64 arrays (flight will be 384 x 175)• Demonstrated 2-D addressing• Implemented light shields• Performed cryogenic life tests• Measured pixel failure rate at end-of-life• Measured open/closed shutter contrast ratio [2,000-
10,000 warm; ~200 cold (due to shutter curvature)]• Performed an acoustic test
01/15/2004 TIPS/JIM MSA Backside
100 m
Magnetic Stripes on MSA Frontside20 m MSA Light Shields
100 m
01/15/2004 TIPS/JIM
Micro-Shutter Array (MSA) Confirmation Review
Concerns:• Yield is still low• Light shields frequently break off• Shutters curve and bend when cooled• Life testing does not meet <10% of rows with a failed-
open shutter• Crude acoustic/shake tests increase rate of failed-opens
Further development needed, but optimism prevails. The MSA remains the preferred approach, and the European
selection is proceeding on this basis.