After working through a few technical difficulties, Northrop Grumman Innovation Systems was ready to launch NASA’s ICON mission aboard its Pegasus XL rocket on Wednesday. However, the attempt was aborted just minutes head of the launch. The air-drop launch of Pegasus XL from underneath the L-1011 Stargazer aircraft was scheduled to occur five minutes after the opening of the launch window – at 03:05 EST (0805 UTC) on Wednesday, 7 November, 200 miles east of Daytona Beach, Florida – prior to an electrical issue forcing another delay.
The road to launch:
The 7 November launch attempt off Central Florida’s east coast came after Northrop Grumman Innovation Systems (NGIS) conducted a captive carry test flight of their Stargazer L-1011 aircraft and Pegasus XL rocket to gather flight data following discovery in late-October of a new issue with the launcher system.
The mission had been on track for a launch on 26 October when the new issue was discovered that forced NGIS to delay launch in order to investigate and fixed the problem.
The issue follows directly behind a previous issue that forced a launch delay back in June after Stargazer, Pegasus XL, and ICON had already left the United States for the Kwajalein Atoll in the South Pacific for launch.
After resolution of June’s actuator issue, NGIS engineers and the flight crew ferried Pegasus XL – with ICON safely inside its payload fairing and Pegasus XL itself securely mounted under Stargazer – to Cape Canaveral Air Force Station, Florida, and the skid strip runway at the Cape.
“Once we [got to the Cape], the guys [performed] the safing operations, [got] all the equipment in place, [got] the ground support equipment, air conditioners, those kind of things ready to go,” said Bryan Baldwin, Pegasus Program Manager, Northrop Grumman Innovation Systems in an interview with NASASpaceflight’s Chris Gebhardt.
“Then, the following day, [we did] what we call a Combined System Test #2 to make sure no issues occurred on the ferry over.” During Combined System Test #2, the teams made sure the hardware on the Stargazer aircraft was ready for launch and that ICON data was available to teams aboard the plane.
During this series of tests, a new issue was discovered within the Stargazer/Pegasus XL/ICON system. Initial notes to L2 after the issue first presented to NGIS engineers revealed that another delay would occur to ICON’s launch – with an exact target launch date initially unavailable as the teams assessed the issue.
After working the issue for a few days, NGIS, in conjunction with NASA, agreed that a captive carry test of Pegasus XL under Stargazer was prudent to gather data on the issue.
.@NASA and @northropgrumman are continuing preparations for the ICON launch. There is range availability Nov. 3-8, and a launch date will be determined after review of data from Sunday's test flight is complete. Details: https://t.co/2RL9zPICKM pic.twitter.com/cKtR44fQ41
— NASA Sun & Space (@NASASun) October 31, 2018
A captive carry test is when the Pegasus XL rocket – with its payload installed – is flown through a launch-day profile to verify all systems aboard the Stargazer L-1011 aircraft, the Pegasus XL rocket, and the ICON payload.
This test serves largely the same purpose as United Launch Alliance’s (ULA’s) Wet Dress Rehearsals of their Atlas V and Delta IV rocket families and SpaceX’s static fire launch pad tests of their Falcon rocket family.
The captive carry occurred from Cape Canaveral over the Atlantic Ocean east of Daytona Beach on Sunday, 28 October.
More than a week of analysis and work on the issue was required before NASA and NGIS convened the Flight Readiness Review on Tuesday, 6 November and formally cleared the ICON mission for launch.
However, the electrical gremlins, as portrayed, returned during the trip to the drop zone, forcing a scrub.
Launch day for ICON began for the NGIS launch control team at 22:50 EST (0350 UTC) when the teams went “on console” 4 hours 15 minutes prior to the targeted “drop time”.
“So the first step [was] the Range facility setup,” said Mr. Baldwin to NASASpaceflight’s Chris Gebhardt in their one-on-one interview. “And then once that [was completed], we [did] what’s called Pegasus Power Up. And we just [powered] up the vehicle and we [sat] there for some time, 45 minutes, letting the engineers review their systems, [making] sure things look as expected.
“We then [got] into a powered systems test, where [we transferred] power from external power supplies to our internal batteries, [made] sure those [were] functioning the way they [were] supposed to and operating nominally.”
After this, a Flight Termination System open-loop test with the Eastern Range was performed before the teams moved into pre-engine start checklist.
Stargazer then started pre-taxi operations 2 hours 15 minutes prior to Pegasus XL launch before taxiing along the runway at the Skid Strip at Cape Canaveral Air Force Station roughly 1 hour 15 minutes prior to drop, after which pre-takeoff checks were performed.
Those checks took about 10 minutes, after which Stargazer powered down the skid strip runway and took off for the drop zone 58 minutes prior to Pegasus XL launch.
After takeoff, Stargazer flew to the launch site located 200 miles east of Daytona Beach, Florida.
The launch window technically opened at 03:00 EST (0800 UTC), but the actual drop launch of Pegasus XL from underneath the L-1011 Stargazer was timed for No Earlier Than 5 minutes into the launch window at 03:05 EST (0805 UTC).
The scrub was called about 20 minutes prior to the window opening.
Had the countdown proceeded, Pegasus XL rocket’s first stage solid motor would have ignited 5 seconds after the rocket dropped from Stargazer, with the entire rocket system then delivering ICON to its 575 km (357 mi) orbit inclined 27° to the equator.
NASA’s Ionospheric Connection Explorer (ICON) satellite is designed to study changes to Earth’s Ionosphere – the ionized part of the upper atmosphere from 60 km to 1,000 km (37 miles to 620 miles) – and interaction between Earth’s weather systems and space weather created by the Sun.
During the course of its mission, ICON will return data to allow scientists to better understand these weather system interactions and how they drive turbulence in the upper atmosphere.
Better understanding this turbulence will allow for improved GPS (Global Positioning System) signals for everyday navigation, improved communications, and an improvement on the technology we rely on every day.
To this end, ICON is part of NASA’s Explorers Program – which traces its roots back to the United States’ very first satellite, Explorer 1, launched on 31 January 1958.
ICON will be the 96th Explorers Program satellite launched and the 16th launched by a Pegasus XL rocket. The last Explorers Program satellite was NASA’s Transiting Exoplanet Survey Satellite (TESS) which launched on a SpaceX Falcon 9 rocket on 18 April 2018.
ICON was formally accepted by NASA on 12 April 2013 and will be operated by the University of California, Berkeley’s Space Sciences Laboratory.
The ICON mission is slated to last two years – during which it will use four instruments to analyze the ionosphere.
1️⃣ gigabit of data per day
— NASA Sun & Space (@NASASun) November 6, 2018
The Ion Velocity Meter (IVM), an ion drift meter, will measure the motion of charged particles in the ionosphere. It was built but the University of Texas, Dallas, and will collect in situ data about ions in the local environment at ICON’s orbital altitude.
Two ultraviolet imagers from UC Berkeley, Extreme Ultra-Violet (EUV) and Far Ultra-Violet (FUV) will observe airglow layers in the upper atmosphere to help characterize ionospheric and thermospheric density and composition.
Finally, the U.S. Naval Research Laboratory built Michelson Interferometer for Global High-Resolution Thermospheric Imaging (MIGHTI) will measure wind speeds and temperatures in the ionosphere between 90 to 300 km (60 – 186 miles).
MIGHTI will gather its velocity data via doppler shifts in the red and green lines of atomic oxygen and is capable of detecting wind speeds as low as 16 kph (10 mph).
ICON is built around a LEOStar-2 buss from NGIS, formerly Orbital ATK, and will be powered by solar panels producing 780 watts – well more than the 209-265 watts consumed by the craft when in full science mode.