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Ignition, lift off, and through booster sep. Trajectory nominal at 163 km.
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal at 163 km.
Stage separation at about 300 km. Onboard cameras showing a glowing Vinci motor.
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal at 163 >>> km.
Stage separation at about 300 km. Onboard cameras showing a glowing Vinci >> motor.
Flight path shown heads up over Scotland. High inclination launched from the
equator!
Snidely is guilty of <mn.4ae07e8735498b78.127094@snitoo> as of 7/9/2024 12:16:35 PM
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal at 163 >>>> km.
Stage separation at about 300 km. Onboard cameras showing a glowing Vinci >>> motor.
Flight path shown heads up over Scotland. High inclination launched from >> the equator!
Past the Azores, and in the initial coast phase at 7.57 km/s.
Snidely asserted that:
Snidely is guilty of <mn.4ae07e8735498b78.127094@snitoo> as of 7/9/2024
12:16:35 PM
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal at 163 >>>>> km.
Stage separation at about 300 km. Onboard cameras showing a glowing
Vinci motor.
Flight path shown heads up over Scotland. High inclination launched from >>> the equator!
Past the Azores, and in the initial coast phase at 7.57 km/s.
Approaching Austalia, with a good circularization burn at 577 km altitude.
Lo, on the 7/9/2024, Snidely did proclaim ...
Snidely asserted that:
Snidely is guilty of <mn.4ae07e8735498b78.127094@snitoo> as of 7/9/2024 >>> 12:16:35 PM
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal at 163 >>>>>> km.
Stage separation at about 300 km. Onboard cameras showing a glowing >>>>> Vinci motor.
Flight path shown heads up over Scotland. High inclination launched from >>>> the equator!
Past the Azores, and in the initial coast phase at 7.57 km/s.
Approaching Austalia, with a good circularization burn at 577 km altitude. >>
9 seconds of cubesat release, roughly over Tasmania.
Snidely formulated the question :
Lo, on the 7/9/2024, Snidely did proclaim ...
Snidely asserted that:9 seconds of cubesat release, roughly over Tasmania.
Snidely is guilty of <mn.4ae07e8735498b78.127094@snitoo> as of
7/9/2024 12:16:35 PM
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal >>>>>>> at 163 km.
Stage separation at about 300 km. Onboard cameras showing a
glowing Vinci motor.
Flight path shown heads up over Scotland. High inclination launched >>>>> from the equator!
Past the Azores, and in the initial coast phase at 7.57 km/s.
Approaching Austalia, with a good circularization burn at 577 km
altitude.
Ooops, there's been a problem with the 2nd stage APU, used for tank
pressure management and engine relight. A planned second boost did not occur, and it appears the stage could not turn to the proper orientation
for the de-orbit burn. More information pending.
On Tue, 09 Jul 2024 14:54:55 -0700, Snidely wrote:
Snidely formulated the question :
Lo, on the 7/9/2024, Snidely did proclaim ...
Snidely asserted that:9 seconds of cubesat release, roughly over Tasmania.
Snidely is guilty of <mn.4ae07e8735498b78.127094@snitoo> as of
7/9/2024 12:16:35 PM
Tuesday, Snidely observed:
Snidely explained on 7/9/2024 :
Ignition, lift off, and through booster sep. Trajectory nominal >>>>>>>> at 163 km.
Stage separation at about 300 km. Onboard cameras showing a
glowing Vinci motor.
Flight path shown heads up over Scotland. High inclination launched >>>>>> from the equator!
Past the Azores, and in the initial coast phase at 7.57 km/s.
Approaching Austalia, with a good circularization burn at 577 km
altitude.
Ooops, there's been a problem with the 2nd stage APU, used for tank
pressure management and engine relight. A planned second boost did not
occur, and it appears the stage could not turn to the proper orientation
for the de-orbit burn. More information pending.
Still and all, much, much better than the first launch of Ariane 5.