Rocket Lab Announces Next Electron Launch Window and Provides Update on Anomaly Review

Rocket Lab Announces Next Electron Launch Window and Provides Update on Anomaly Review

Rocket Lab USA, one of the global leaders in launch services and space systems, announced it has set a return to launch window for its Electron launch vehicle. Rocket Lab will return to the pad at Launch Complex 1 with a dedicated Electron mission for Japan-based Earth imaging company iQPS (Institute for Q-shu Pioneers of Space) during a launch window that opens on November 28th, 2023, and extends into December.

The resumption of Electron launches comes as Rocket Lab approaches the conclusion of an extensive review into the cause of the anomaly that resulted in the loss of its 41st Electron mission launched on September 19th, 2023. The anomaly occurred after 20 consecutive successful orbital missions and 37 successful Electron missions overall for government and commercial satellite operators, with 171 satellites deployed to orbit.

The September 19th mission completed lift-off, clearance through Max Q, and stage separation between the rocket’s first and second stage. At 151 seconds into the mission, the high voltage from the second stage’s power supply system anomalously fell sharply. In less than a second, the stage experienced a total loss of power and was unable to reach orbital velocity to deliver the mission’s payload, subsequently re-entering the atmosphere and ending the mission. In accordance with Rocket Lab’s safety protocols, public safety was not affected.

After more than seven weeks of extensive analysis of the mission’s manufacturing, test, and flight data, the findings of the investigation overwhelmingly indicate that an unexpected electrical arc occurred within the power supply system that provides high voltage to the Rutherford engine’s motor controllers, shorting the battery packs that provide power to the launch vehicle’s second stage.

Exhaustive testing and analysis to recreate this failure mode has led to the investigation team’s determination that the arc was likely only made possible by the rare interaction of multiple conditions. Any one of these factors on their own would likely not have caused the failure of the second stage, but when they occur simultaneously in the low-pressure environment of space, they reach the threshold dictated by Paschen’s Law for an arc to form and travel. Paschen's Law is an equation that breaks down the relationship between voltage, pressure environment, distance between electrodes, and the presence of gas necessary for an electrical arc to form and travel.

Three rare conditions had to present simultaneously in the low-pressure space environment to reach the threshold for arcing under Paschen’s Law, including:

  • A superimposed alternating current (AC) with the direct current (DC) high-voltage electricity provided to the stage’s power supply system, that is produced as a ripple voltage from the system’s engine motor controllers;
  • A small concentration of helium and nitrogen gasses that were present within the interstage between Electron’s first and second stages; and
  • An imperceptible fault in the insulation of the high voltage loom within the power supply system.

These factors combined, including electricity in the presence of both helium and nitrogen, while under a partial pressure environment, unrestrained by a fault in the high voltage loom, and exacerbated by an alternating current, aligned at a point on the Paschen curve that allows an electrical arc to form and travel.

This highly complex set of conditions is extremely difficult to predict and test for on Earth, even in simulated space conditions. To ensure the fault does not present again, Rocket Lab is implementing two key corrective measures -- one designed to improve testing on the ground and another to eliminate the possibility of comparable arcs occurring in flight should similar faults evade the new enhanced testing process.

While pre-launch testing of the second stage’s power supply system already covers the full range of its operational parameters including pressure, ionization levels, and voltage, the enhanced test routine will now account for even harsher conditions than those experienced in space, including increasing test-to-flight margins and flight-representative voltage waveforms.

As an additional redundancy feature, Rocket Lab has modified Electron’s battery frame section which houses the high voltage power supply system to enable it to maintain optimum gaseous pressure from launch through to stage separation from Electron’s Kick Stage. Pressurizing this section significantly reduces the ability for arcs to form.

Rocket Lab founder and CEO Peter Beck said: "This is a highly complex, improbable, and evasive issue that the team has been relentless in investigating and fixing so we can put an even better vehicle back on the pad. We are grateful to our customers and the FAA for their continued support through this thorough investigation process. Thank you for your trust in our team. We look forward to returning to flight with corrective measures in place to provide the frequent and reliable access to orbit that the industry has come to depend on after 37 successful Electron missions."

Rocket Lab expects to formally close its anomaly investigation in the coming weeks. Rocket Lab has also already received authorization from the Federal Aviation Administration (FAA) to resume Electron launches from Launch Complex 1.

Click here to learn more about Rocket Lab's upcoming missions.

Publisher: SatNow
Tags:-  SatelliteLaunchGround

GNSS Constellations - A list of all GNSS satellites by constellations

beidou

Satellite NameOrbit Date
BeiDou-3 G4Geostationary Orbit (GEO)17 May, 2023
BeiDou-3 G2Geostationary Orbit (GEO)09 Mar, 2020
Compass-IGSO7Inclined Geosynchronous Orbit (IGSO)09 Feb, 2020
BeiDou-3 M19Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M20Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M21Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 M22Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 I3Inclined Geosynchronous Orbit (IGSO)04 Nov, 2019
BeiDou-3 M23Medium Earth Orbit (MEO)22 Sep, 2019
BeiDou-3 M24Medium Earth Orbit (MEO)22 Sep, 2019

galileo

Satellite NameOrbit Date
GSAT0223MEO - Near-Circular05 Dec, 2021
GSAT0224MEO - Near-Circular05 Dec, 2021
GSAT0219MEO - Near-Circular25 Jul, 2018
GSAT0220MEO - Near-Circular25 Jul, 2018
GSAT0221MEO - Near-Circular25 Jul, 2018
GSAT0222MEO - Near-Circular25 Jul, 2018
GSAT0215MEO - Near-Circular12 Dec, 2017
GSAT0216MEO - Near-Circular12 Dec, 2017
GSAT0217MEO - Near-Circular12 Dec, 2017
GSAT0218MEO - Near-Circular12 Dec, 2017

glonass

Satellite NameOrbit Date
Kosmos 2569--07 Aug, 2023
Kosmos 2564--28 Nov, 2022
Kosmos 2559--10 Oct, 2022
Kosmos 2557--07 Jul, 2022
Kosmos 2547--25 Oct, 2020
Kosmos 2545--16 Mar, 2020
Kosmos 2544--11 Dec, 2019
Kosmos 2534--27 May, 2019
Kosmos 2529--03 Nov, 2018
Kosmos 2527--16 Jun, 2018

gps

Satellite NameOrbit Date
Navstar 82Medium Earth Orbit19 Jan, 2023
Navstar 81Medium Earth Orbit17 Jun, 2021
Navstar 78Medium Earth Orbit22 Aug, 2019
Navstar 77Medium Earth Orbit23 Dec, 2018
Navstar 76Medium Earth Orbit05 Feb, 2016
Navstar 75Medium Earth Orbit31 Oct, 2015
Navstar 74Medium Earth Orbit15 Jul, 2015
Navstar 73Medium Earth Orbit25 Mar, 2015
Navstar 72Medium Earth Orbit29 Oct, 2014
Navstar 71Medium Earth Orbit02 Aug, 2014

irnss

Satellite NameOrbit Date
NVS-01Geostationary Orbit (GEO)29 May, 2023
IRNSS-1IInclined Geosynchronous Orbit (IGSO)12 Apr, 2018
IRNSS-1HSub Geosynchronous Transfer Orbit (Sub-GTO)31 Aug, 2017
IRNSS-1GGeostationary Orbit (GEO)28 Apr, 2016
IRNSS-1FGeostationary Orbit (GEO)10 Mar, 2016
IRNSS-1EGeosynchronous Orbit (IGSO)20 Jan, 2016
IRNSS-1DInclined Geosynchronous Orbit (IGSO)28 Mar, 2015
IRNSS-1CGeostationary Orbit (GEO)16 Oct, 2014
IRNSS-1BInclined Geosynchronous Orbit (IGSO)04 Apr, 2014
IRNSS-1AInclined Geosynchronous Orbit (IGSO)01 Jul, 2013