Flight Profile - Vega VV10
(VENµS & OPTSAT-3000)
Launch Timeline
Time | Event |
---|---|
T-0:04:00 | Start of Synchronized Sequence |
T-0 | P80 First Stage Ignition & Liftoff |
T+0:01:57 | P80 Separation |
T+0:01:58 | Zefiro-23 Second Stage Ignition |
T+0:03:40 | Zefiro-23 Separation |
T+0:04:03 | Zefiro-9 Third Stage Ignition |
T+0:04:08 | Payload Fairing Separation |
T+0:06:42 | Zefiro-9 Separation |
T+0:07:52 | AVUM - 1st Main Engine Start |
T+0:07:52 | Burn Duration: 6 Min & 17 Sec |
T+0:14:09 | AVUM - 1st Shutdown |
T+0:40:37 | AVUM - 2nd Main Engine Start |
T+0:40:37 | Burn Duration: 1 Min & 25 Sec |
T+0:42:02 | AVUM - 2nd Shutdown |
T+0:42:49 | OPTSAT-3000 Separation |
T+0:52:04 | Separation of VUP Adapter |
T+0:53:05 | AVUM - 3rd Main Engine Start |
T+0:53:05 | Burn Duration: 58 Seconds |
T+0:54:03 | AVUM - 3rd Shutdown |
T+1:35:20 | AVUM - 4th Main Engine Start |
T+1:35:20 | Burn Duration: 1 Min & 4 Sec |
T+1:36:24 | AVUM - 4th Shutdown |
T+1:37:17 | VENµS Separation |
T+1:47:19 | AVUM - 5th Main Engine Start (Deorbit) |
T+1:48:37 | AVUM - 5th Shutdown |
Launch Info
Launch Vehicle: Vega
Launch Site: ZLV, Guiana Space Center
Launch Date: August 2, 2017
Launch Time: 01:58:33 UTC
Payloads: OPTSAT-3000, VENµS (632 kg)
Mission Duration: 1 Hour & 37 Minutes
Target Orbits
OPTSAT-3000:
Type: Sun Synchronous Orbit
Altitude: 450 Kilometers
Inclination: 97°
VENµS:
Type: Sun Synchronous Orbit
Altitude: 720 Kilometers
Inclination: 98°
Payload Configuration


VV10 Flight Profile - Image: Arianespace