837095c6390ee9493e66d5de27386b78d597bbc34ba6eebbff3692c10685768f2026 AUD.This is a program-framing ROM. It is not a supplier quote, an independently validated cost estimate, or an approved funding or schedule baseline.
| Case | WBS base (M AUD) | Reserve | Reserve (M AUD) | Total (M AUD) |
|---|---|---|---|---|
low |
544.00 |
15.0% |
81.60 |
625.60 |
planning |
809.00 |
25.0% |
202.25 |
1011.25 |
high |
1218.00 |
40.0% |
487.20 |
1705.20 |
| ID | Work package | Released subsystems | Basis type | Low / planning / high (M AUD) | Owner |
|---|---|---|---|---|---|
CST-01 |
Program management, systems engineering, safety, mission assurance, and product assurance | cross-cutting | engineering_judgement |
45.0 / 65.0 / 95.0 |
program manager |
CST-02 |
Optical payload and detector development | optics, detector | engineering_judgement |
90.0 / 140.0 / 220.0 |
payload lead |
CST-03 |
Structures and deployment mechanisms | structures_and_mechanisms | engineering_judgement |
35.0 / 55.0 / 90.0 |
mechanical lead |
CST-04 |
Thermal-control subsystem | thermal_control | engineering_judgement |
20.0 / 32.0 / 50.0 |
thermal lead |
CST-05 |
Electrical power subsystem | power | engineering_judgement |
18.0 / 28.0 / 45.0 |
electrical power lead |
CST-06 |
Propulsion subsystem | propulsion | engineering_judgement |
15.0 / 25.0 / 40.0 |
propulsion lead |
CST-07 |
Attitude determination and control subsystem | adcs | engineering_judgement |
20.0 / 32.0 / 50.0 |
GNC lead |
CST-08 |
Command and data handling subsystem | cdh | engineering_judgement |
15.0 / 24.0 / 38.0 |
avionics lead |
CST-09 |
RF communications subsystem | communications | engineering_judgement |
18.0 / 28.0 / 45.0 |
RF lead |
CST-10 |
Flight software and FDIR | flight_software | engineering_judgement |
25.0 / 40.0 / 65.0 |
flight software lead |
CST-11 |
Assembly, integration, verification, GSE, and facilities | cross-cutting | planning_allowance |
45.0 / 70.0 / 110.0 |
AIV manager |
CST-12 |
Ground segment and mission-operations preparation | cross-cutting | planning_allowance |
18.0 / 30.0 / 50.0 |
mission operations manager |
CST-13 |
Launch service, mission-specific launch integration, and insurance allowance | cross-cutting | planning_allowance |
180.0 / 240.0 / 320.0 |
launch services manager |
72.0.9.0 months
(12.5% of the baseline development span).81.0.84.0.| Phase | Months | Critical path | Predecessors | Owner | Exit evidence |
|---|---|---|---|---|---|
SCH-01 Requirements maturation and system
definition |
0-9 |
yes | none | chief systems engineer | System requirements review closes the mission, interface, verification, cost, and schedule baselines for preliminary design. |
SCH-02 Preliminary design and technology-risk
retirement |
9-21 |
yes | SCH-01 | chief engineer | Preliminary design review closes subsystem allocations, credible interfaces, breadboard evidence, and long-lead release authority. |
SCH-03 Detailed design and engineering-model
release |
21-39 |
yes | SCH-02 | chief engineer | Critical design review releases controlled drawings, software architecture, procurement data, and engineering-model configurations. |
SCH-04 Engineering and qualification articles |
39-54 |
yes | SCH-03 | qualification manager | Qualification readiness review confirms representative articles, facilities, GSE, procedures, and non-conformity control are ready. |
SCH-05 Flight manufacture and observatory
integration |
54-66 |
yes | SCH-04 | AIV manager | Integrated flight observatory completes functional, alignment, workmanship, and configuration audits before acceptance testing. |
SCH-06 Environmental acceptance and launch
readiness |
66-72 |
yes | SCH-05 | mission assurance manager | Acceptance campaign, end-to-end mission rehearsal, shipment review, and launch readiness review close without open flight-critical waivers. |
SCH-07 Launch campaign and commissioning |
81-84 |
no | SCH-06 | mission director | Launch, early operations, deployment, calibration, and commissioning acceptance establish the released nominal-science configuration. |
| ID | Milestone | Month | Phase |
|---|---|---|---|
MS-SRR |
System requirements review complete | 9 |
SCH-01 |
MS-PDR |
Preliminary design review complete | 21 |
SCH-02 |
MS-CDR |
Critical design review complete | 39 |
SCH-03 |
MS-QRR |
Qualification readiness review complete | 54 |
SCH-04 |
MS-FIR |
Flight integration complete | 66 |
SCH-05 |
MS-LRR |
Launch readiness review complete | 72 |
SCH-06 |
MS-LAUNCH |
Commitment launch milestone | 81 |
SCH-07 |
MS-COMMISSION |
Commissioning acceptance complete | 84 |
SCH-07 |
| ID | Risk | Cost WBS | Schedule phases | Owner | Treatment |
|---|---|---|---|---|---|
RSK-01 |
Primary-mirror fabrication yield or detector procurement extends the payload critical path and forces replacement hardware. | CST-02 | SCH-02, SCH-03, SCH-04 | payload lead | Retire mirror-process and detector-supply risks before PDR, preserve qualification spares, and gate flight procurement on representative evidence. |
RSK-02 |
Deployment mechanism life testing exposes release, synchronization, routing, or retained-capture redesign. | CST-03, CST-11 | SCH-03, SCH-04 | mechanical lead | Build representative mechanism articles early, test across thermal extremes, and preserve schedule for redesign before flight manufacture. |
RSK-03 |
Fine-pointing and wheel-induced jitter exceed the optical line-of-sight allocation during integrated testing. | CST-07, CST-11 | SCH-02, SCH-03, SCH-04 | GNC lead | Add disturbance testing and integrated structural-optical correlation before CDR and retain isolation design authority. |
RSK-04 |
Environmental or end-to-end acceptance failures require observatory disassembly and repeat testing. | CST-01, CST-11 | SCH-05, SCH-06 | mission assurance manager | Use qualification articles, incremental workmanship tests, controlled non-conformity closure, and explicit test-repeat allowances. |
RSK-05 |
Ground-station access, licensing, or interface work differs from the representative two-site CONOPS. | CST-09, CST-12 | SCH-02, SCH-03, SCH-05 | mission operations manager | Secure network agreements and regulatory strategy before PDR and validate RF and mission-control interfaces with representative ground equipment. |
RSK-06 |
Launch-service contracting, rideshare allocation, or mission-specific integration differs from the internal Ariane 6 allowance. | CST-13 | SCH-02, SCH-05, SCH-06 | launch services manager | Obtain provider budgetary data during formulation, preserve interface-change control, and carry cost and schedule reserves until contract signature. |
RSK-07 |
Radiation-tolerant avionics lead times or obsolescence force C&DH, power, RF, or software rework. | CST-05, CST-08, CST-09, CST-10 | SCH-02, SCH-03, SCH-05 | avionics lead | Freeze the approved-parts strategy early, procure engineering lots before CDR, and maintain compatible alternates. |
RSK-08 |
Specialised cleanroom, thermal-vacuum, vibration, acoustic, shock, or optical-alignment facilities are unavailable at the planned dates. | CST-11 | SCH-03, SCH-04, SCH-06 | AIV manager | Place provisional facility reservations during preliminary design and qualify alternate facilities and transport plans before CDR. |
| Check | Result |
|---|---|
cost_schedule_policy_schema_supported |
PASS |
cost_schedule_basis_matches_released_program |
PASS |
cost_schedule_upstream_release_evidence_passes |
PASS |
cost_wbs_ranges_and_reserves_are_complete |
PASS |
cost_wbs_covers_every_released_subsystem_once |
PASS |
schedule_logic_reserve_and_subsystem_coverage_close |
PASS |
schedule_milestones_match_phase_and_commitment_boundaries |
PASS |
cost_schedule_risk_drivers_are_owned_and_traceable |
PASS |