Seagate Space is developing its offshore launch infrastructure system from the ground up rather than retrofitting existing vessels.

Project Manta is Space Florida’s first maritime-based launch infrastructure initiative.

FTW provides an API and a command-line tool for more complex workflows.

The FTW online platform lets users generate field boundaries using recent Sentinel-2 imagery.

Fields of The World (FTW) is a global project developed by Taylor Geospatial, NASA Harvest, Microsoft AI for Good Lab, the Arizona State University, Washington University in St. Louis, and Clark University.

The FTW Explorer app lets users draw an area, run field-boundary detection, and download the results.

The FTW release includes confidence levels that let users adjust how conservative or inclusive the results are.

SD Government, a Gogo company focused on military and government markets, has secured a multi-year blanket purchase agreement with NOAA to support airborne hurricane hunting activities via satellite communications ahead of the 2026 hurricane season.

The NOAA agreement will support NOAA’s Aircraft Operations Center, which operates the Hurricane Hunter fleet.

The NOAA agreement carries a total obligation of $7.5 million.

NOAA’s Hurricane Hunter fleet includes the Lockheed Martin WP-3D aircraft known as Kermit and Miss Piggy.

Under the NOAA contract, SD Government will provide an L-band satellite communications service, associated ground infrastructure, and cybersecurity services through Gogo’s data center in Melbourne, Florida.

The NOAA contract also includes Gogo’s FlightDeck Freedom cockpit datalink software suite.

INNOSPACE is undergoing review with the Korea AeroSpace Administration to obtain launch authorisation for a follow-up HANBIT-Nano launch.

INNOSPACE plans a follow-up HANBIT-Nano launch in the third quarter of this year, subject to final approval.

INNOSPACE developed a bi-propellant regenerative cooling approach for methane engine combustors.

INNOSPACE plans to integrate its 0.4-ton thrust liquid methane engine, LiMEK-04, into the kick stage of its next-generation HANBIT-Micro launch vehicle.

INNOSPACE identified the root cause of the HANBIT-Nano mission failure, upgraded components, and optimized manufacturing processes.

INNOSPACE completed a 420-second ground firing test for its methane engine combustor.

INNOSPACE is undergoing review with the Korea AeroSpace Administration to obtain launch authorisation for HANBIT-Nano.

INNOSPACE said the bi-propellant architecture can enable lighter tanks and feed systems.

INNOSPACE’s bi-propellant cooling approach uses both liquid methane and liquid oxygen as coolants for the combustion chamber.

INNOSPACE has developed a bi-propellant regenerative cooling approach for methane engine combustors.

INNOSPACE is continuing development of the HANBIT-Micro combustor with liquid oxygen as a coolant.

INNOSPACE conducted a 237-second ground firing test in May 2024 on the 0.4-ton thrust methane engine combustor for the HANBIT-Micro kick stage.

INNOSPACE identified the root cause of the early termination of its first commercial launch mission, HANBIT-Nano, and upgraded components and manufacturing processes.

INNOSPACE has continued developing the HANBIT-Micro combustor with liquid oxygen as a coolant.

The 420-second ground firing test was the longest domestic burn for this class of combustor.

INNOSPACE’s first commercial launch mission, HANBIT-Nano, ended early in December 2025.

INNOSPACE’s bi-propellant cooling approach uses liquid methane and liquid oxygen as coolants for the combustion chamber.

INNOSPACE said the bi-propellant architecture increases coolant flow rate by about 3.0 to 3.4 times compared with conventional approaches.

The bi-propellant architecture is intended to allow stable cooling under lower pressure conditions and enable lighter tanks and feed systems.

INNOSPACE plans to integrate LiMEK-04 into the kick stage of its next-generation HANBIT-Micro launch vehicle.

INNOSPACE completed a 420-second ground firing test for the methane engine combustor, which it described as the longest domestic burn for this class of combustor.

INNOSPACE’s cooling technology is intended for its 0.4-ton thrust liquid methane engine, LiMEK-04.

INNOSPACE previously conducted a 237-second ground firing test in May 2024 on the 0.4-ton thrust methane engine combustor for the HANBIT-Micro kick stage.

Michelangelo Moles holds a master’s degree in Corporate Communication and Media.

Kaman’s Advanced Magnetic Sensing technology measures mechanical runout, rotational speed, and machine vibration profiles.

Kaman’s Advanced Magnetic Sensing systems provide root mean square resolution down to a single micron and a standard measuring range of up to seven millimeters.

Kaman’s Advanced Magnetic Sensing systems operate from -320°F to +1000°F, with short-term tolerances up to +1200°F.

Kaman’s non-contact measuring systems work with any ferromagnetic target and can detect positions through non-magnetic, conductive, and non-conductive barriers.

Kaman’s Advanced Magnetic Sensing systems operate in high-pressure environments from 500 psi to 40,000 psi.

Kaman’s Advanced Magnetic Sensing systems are engineered for aerospace propulsion applications.

Kaman Precision Products’ Measuring Division has an Advanced Magnetic Sensing family of high-precision non-contact measuring systems.

Kaman’s IP-67 rated sensors are available with threaded, flanged, bolt head, and AS4320 pressure port-compatible configurations.

Kaman’s sensors can detect non-contact speed sensing, shaft runout, and gear tooth conditions in real time.

Kaman provides displacement measurement systems for ground testing facilities, rocket engines, and operational satellites.

LandSpace conducted a pad-transporter rehearsal with a mock-up before the ZQ-3 Y2 launch.

Engineers completed Long March 12B development from initial design studies to final product development in 21 months.

The first Long March 12B rocket carried Qianfan constellation satellites.