When (first) orbital flight?First integrated flight test occurred April 20, 2023. "The vehicle cleared the pad and beach as Starship climbed to an apogee of ~39 km over the Gulf of Mexico – the highest of any Starship to-date. The vehicle experienced multiple engines out during the flight test, lost altitude, and began to tumble. The flight termination system was commanded on both the booster and ship."
What's happening next? SpaceX has assessed damage to Stage 0 and is implementing fixes and changes including a water deluge/pad protection/"shower head" system. No major repairs to key structures appear to be necessary.
Why no flame diverter/flame trench below the OLM?Musk tweeted on April 21: "3 months ago, we started building a massive water-cooled, steel plate to go under the launch mount. Wasn’t ready in time & we wrongly thought, based on static fire data, that Fondag would make it through 1 launch." Regarding a trench, note that the Starship on the OLM sits 2.5x higher off the ground than the Saturn V sat above the base of its flame trench, and the OLM has 6 exits vs. 2 on the Saturn V trench.
I copied and pasted it here. Thanks to @[email protected] for pointing me back at the RES extension so I could get the source.
Each item is on its own line. C## is the ID#. If there's text before it on its line, that's its Observation / Description section name; if it's at the start of the line, the Observation / Description string is the next one above.
List of Actions:
Observation / Description
ID#
Corrective Action Description
Status
Tank sensing
C1
Replace certain fittings with welds inside tank
Complete
Aft end cavity environment failure
C2
Increase fire suppression capacity by 15x
Complete
C3
Replace certain manifolds with dedicated drain per corresponding valve
Complete
C4
Replace certain flanges with better seals and improve joint design
Complete
C5
Replace certain fittings with welds in specific location
Complete
Booster leak
C6
Replace accessible valves of a certain type with new design
Complete
mitigation
C7
Replace certain flange bolts with higher strength bolts and increase torque
Complete
C8
Disallow certain seal re-use, and add cameras to monitor all engines during ground operations
Complete
C9
Increased scrutiny on leak checks
Complete
C10
90+ cameras added to detect leakage during operations
Complete
C11
Add leak capture and drain hardware for valves of a certain type
Complete
C12
Add leak check and screen for porosity on igniter units
Complete
C13
Improved igniter seal design
Future Action
C14
Weld certain alignment bolt holes shut
Complete
Raptor leak
C15
Reassess k-factor and torque for engine hot joint #1, add leak capture and route overboard
Complete
mitigation
C16
Reassess k-factor and torque for engine hot joint #2
Complete
C17
Add safety cable to certain fluid lines on high risk locations
Complete
C18
Add one methane sensor per engine bay
Complete
C19
Ground test campaign to better characterize typical engine leakage
Complete
C20
Improve structural FEA/fatigue analysis for all medium to high criticality lines
Complete
C21
Add insulation to engine lines sensitive to thermally driven loads
Complete
Collateral
C22
Add insulation to avionic harnessing
Complete
damage from fire
C23
Add backup wire to specific harness
Complete
C24
Improve thermal protection of avionics tray
Complete
C25
Change routing to flight computers
Complete
C26
Replace sensor with more reliable units
Complete
C27
Coat gimbal assembly with lubricant
Complete
C28
Add pump pressure sensors to certain location
Complete
C29
Add pump temperature sensors to certain location
Complete
Booster reliability
C30
Replace certain bolts, and increase torque for certain flanges
Complete
improvement
C31
New seal design for certain areas of booster
Complete
C32
Add electric actuation system
Complete
C33
Better manage engine bay pressure by increasing fire suppression capacity by
Complete
C34
Change certain booster valve timing
Future Action
C35
Add final leak checks for critical joints
Complete
C36
Add support bracket for certain sensor
Complete
C37
Add support bracket for certain sensor
Complete
C38
Add check valves to certain areas of engine
Complete
C39
Improve oxygen valve design
Future Action
C40
Improve oxygen valve seal design
Future Action
Raptor reliability
C41
Improve design of hot manifold
Future Action
improvement
C42
Change nitrogen shutdown usage
Complete
C43
Change engine shutdown logic
Complete
C44
Increase capability for ground leakage mitigation
Complete
C45
Redesign fire suppression system
Complete
C46
Change conditions around bolts
Complete
C47
Change timing of specific valve actuation
Complete
Avionics reliability
C48
Eliminate certain type of connector
Complete
improvement
C49
Redesign network architecture
Future Action
Risk Process
C50
Improve risk tracking process
Complete
C51
Implement improvements to safety system
Complete
Safety System
C52
Verify flight safety system design improvements using additional type of test article
Complete
C53
Verify flight safety system design improvements via analysis
Complete
C54
Perform component testing
Complete
C55
Review and improve operations surrounding flight safety system