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Suborbital Test of NASA-Supported Payloads, Student Experiments

The National Aeronautics and Space Administration is America’s civil space program and the global leader in space exploration. The agency has a diverse workforce of just under 18,000 civil servants, and works with many more U.S. contractors, academia, and international and commercial partners to explore, discover, and expand knowledge for the benefit of humanity.


Launched on Thursday, September 18, 2025, at Blue Origin’s Launch Site One in West Texas, this flight test is helping researchers from NASA, universities, and private companies advance solutions that will help inform the agency’s lunar exploration through missions like Artemis, and future Mars missions. Also aboard Blue Origin’s New Shepard vehicle: 24 experiments from NASA’s TechRise Student Challenge, which fosters the U.S. space industry through use of commercial vehicles for flight tests, while also strengthening the space technology researcher community by providing a hands-on opportunity for middle and high school students to gain critical skills in engineering, computing, electronics, and more. The 2025-2026 TechRise is open for students to submit ideas from September 4 to November 3, 2025 — see below for more information.

Read more about the technologies, instruments, and experiments on the manifest about

Flight Provider

Blue Origin

Flight Test Platform

Reusable suborbital rocket system

Number of NASA-Supported Payloads

14 from researchers
24 from TechRise students

Flight Date

September 18, 2025

What’s on the Manifest

Advanced Power and Thermals | Biological and Physical Sciences | Cryogenic Fluid Management | In-Situ Resource Utilization | In-Space Servicing, Assembly & Manufacturing | Landing Systems and Environments | Observation Systems | Surface Habitation Systems | Learning with NASA

Advanced Power and Thermals

About the PayloadImpact/Potential UsesFlight Test Goals

Gravity Effects on Electrically Driven Liquid Film BoilingWorchester Polytechnic Institute / NASA’s Goddard Space Flight Center

This gravity-independent hardware improves two-phase heat transfer by providing a constant liquid working fluid source through electrohydrodynamic (EHD) conduction pumping and extracting the vapor bubbles away from the heated surface during the boiling with di-electrophoretic (DEP) force.This thin-film boiling technology is a thermal management system that acquires heat at higher fluxes while consuming less power than other systems, benefiting a wide variety of NASA and commercial spacecraft. To determine the combined effect of EHD and DEP force on boiling heat transfer under varying gravity to validate experiment hardware for applications in NASA’s various missions as well as in next-generation cooling technology for satellites


Hydrogen Electrical Power System (HEPS)
Teledyne Energy Systems, Inc.

This primary fuel cell system is designed to convert hydrogen and oxygen into water and electricity. Teledyne’s ejector-driven reactant (EDR) fuel cell system is a cost-effective and efficient way to supply power in space since it can reduce launch mass and contribute to a sustained human presence in space. Teledyne previously advanced the water separation subsystem aboard parabolic flights.NASA provided a Tipping Point award and access to facilities and expertise at Glenn Research Center because all space missions require power, and fuel cell systems are an integral part of the solution. Teledyne’s EDR system is capable of providing continuous power when sunlight is not available and is extremely scalable, meaning it can power a small experiment or a large lunar base.To demonstrate operation of the system in a space environment, validate water separation in microgravity, and generate data to advance the system for future space missions.

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Biological and Physical Sciences

About the PayloadImpact/Potential UsesFlight Test Goals

Biological Imaging in Support of Suborbital ScienceUniversity of Florida

This flexible imaging system for exploration science aims to autonomously provide high-resolution data for a variety of biological payloads during transitions in gravity levels. This capability could facilitate collection of morphometric (i.e., shape/form-related), gene expression, and biochemical responses through fluorescent biosensors.This system addresses the need for state-of-the-art images for government, academic, and commercial biological research as well as biological studies to understand orbital and beyond low Earth orbit environments.

To perform high-fidelity testing of the camera’s systems during microgravity to inform development for low Earth orbit and other environments

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Cryogenic Fluid Management

About the PayloadImpact/Potential UsesFlight Test Goals

Non-invasive Detection of Liquid Propellant Location During Microgravity Transfer (MPG-MUD) • Carthage College

Designed to facilitate the transfer/storage of cryogenic and other propellants in microgravity, this technology uses external piezoelectric sensors to translate acoustic vibrations applied to the tank into electric voltages, helping determine the total liquid volume and location/motion of the liquid-free surface inside.This system offers a solution for improved propellant management for refueling and other in-space propulsion applications.To help verify sensor operation in a relevant space environment, correlating liquid-free surface position and motion with sensor amplitudes

Propellant Gauging During On-Orbit Refueling and Transfer Operations (MPG-PROTO)Carthage College

In-space propellant transfers require accurate microgravity liquid mass gauging. This modal propellant gauging (MPG) technique translates measured modal frequencies and mode shapes to precisely estimate propellant quantity.The MPG is designed to reduce risk and enable extended human presence on lunar surfaces. Future users include commercial and military satellite and launch service providers, NASA and commercial programs developing in-orbit fuel depots.To test the ability to gauge equilibrated liquids in microgravity during continuous transfer

Spacecraft On-Orbit Advanced Refueling and Storage (SOARS)Eigen Strategies

The SOARS controlled-gravity fluid transfer system is designed to enable precision fluid management in microgravity environments, providing a foundational technology for controlled phase separation and fluid transfer to a variety of operations that require precise fluid control in microgravity.The SOARS system aims to support on-orbit propellant storage and transfer as well as applications such as pharmaceutical synthesis, advanced materials processing, space mining operations, and regolith processing for in-situ resource utilization.To validate controlled gravity fluid separation dynamics and transfer capabilities in microgravity, demonstrating rotational settling techniques and precision flow control

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In-Situ Resource Utilization

About the PayloadImpact/Potential UsesFlight Test Goals

Honey Bubble Excitation Experiment (H-BEE) for Lunar Molten Regolith Analog DemonstrationHoneybee Robotics Ltd.

This system will test the physics of bubble formation and transportation in viscous fluid in reduced and microgravity. This payload has also been tested on a lunar gravity suborbital flight.Results will be used to study bubbles in viscous fluid, which could help inform the design of both in-situ resource extraction and life support systems.To characterize bubble formation and transportation in viscous fluid in microgravity, using a simple and reusable platform

Multiphase Microfluidics for Chemical Analysis SystemsNASA’s Jet Propulsion Laboratory

Designed to assess multi-phase reservoirs for sample mixing and bubble migration, the FORGE (Fluidic Operations in Reduced Gravity Experiments) sample handling system uses reservoirs’ shapes and a magnetic field to help drive the gas phase to desired locations and prevent bubbles from blocking channels.The FORGE technology could benefit NASA missions as well as the commercial space industry.To demonstrate that end-to-end fluidic systems, including multiphase reservoirs, are suitable for chemical analysis missions at any gravity level

Soil Properties Assessment, Resistance, and Thermal Analysis (SPARTA)NASA’s Jet Propulsion Laboratory

Designed to sense small concentrations of subsurface water, SPARTA is a versatile, miniature, multi-tool instrument that provides in-situ measurements of regolith densities as well as geomechanical, thermal, electrical, and chemical properties of soils and permanently frozen layers on planetary surfaces.The SPARTA instrument could prove useful for in-situ lunar missions, data collection for fundamental science, and ground truthing for NASA’s in-situ resource utilization activities.To improve the ability to calibrate SPARTA and determine how various gravities affect shear, penetration resistance, and dielectric properties

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In-Space Servicing, Assembly & Manufacturing

About the PayloadImpact/Potential UsesFlight Test Goals

 In-Space Biosensors Batch Coating Using Self-Assembled MonolayersEcoatoms, Inc.

This project aims to determine whether microgravity allows for the creation of better, more uniform, and smoother coatings that could increase the sensitivity and specificity of electrochemical biosensors — analytical point-of-care diagnostics tools that can rapidly and cost-effectively detect a broad range of molecular analytes. The payload, known as ARES (Advanced Reinforced Engineering Structure), also includes Ecoatoms’s TechLeap Prize-winning universal connector system known as ANIMA.Addressing the uniformity and smoothness of the real-time biosensor’s self-assembled monolayer could benefit on-orbit manufacturing of point-of-care diagnostics, sensors, and biomarker detection devices for use during long-duration flights as well as here on Earth.To demonstrate an automated batch system for sensor coating and fabrication to address challenges of accuracy and reproducibility

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Landing Systems and Environments

About the PayloadImpact/Potential UsesFlight Test Goals

Dust In-Situ Manipulation System (DIMS)University of Central Florida

Designed to overcome current limitations related to the levitation of dust clouds in microgravity, DIMS enables observation of undisturbed dust clouds from two different angles using high-speed cameras to create a 3D image of the cloud.The scientific investigation of dust particles is crucial to understanding the environments of planetary bodies.  Future uses could include solar system exploration and utilization programs for NASA and the commercial space industry as well as scientific research.To determine and demonstrate the system’s ability to create and control clouds of dust in microgravity

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Observation Systems

About the PayloadImpact/Potential UsesFlight Test Goals

JANUS-TEC: for Atmospheric Observational CapabilityJohns Hopkins University (JHU) Applied Physics Laboratory (APL)

As part of the previously tested JHU APL Integrated Universal Suborbital (JANUS) platform, which is designed to integrate sensors for observing spaceflight conditions during suborbital flight altitudes, JANUS-TEC aims to accurately perform total electron content (TEC) observations of the ionosphere while integrated into a reusable suborbital rocket.This technology could offer insight into Earth’s ionosphere; provide low-cost, ride-along measurements; and improve the accuracy of communications and navigation systems, with measurements benefitting research institutions; atmospheric, ionospheric, and heliospheric scientists; spacecraft providers; and other organizational suborbital flights.To establish, evaluate, and verify the TEC observational capability of the JANUS platform

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Surface Habitation Systems

About the PayloadImpact/Potential UsesFlight Test Goals

Ionizing Radiation Dosimeters  for Use in the Upper AtmosphereOklahoma State University

This EPSCoR (Established Program to Stimulate Competitive Research) project is evaluating the ability of several radiation-measuring dosimeters to operate continuously and successfully during the entirety of a suborbital rocket-powered flight.This effort to better understand atmospheric radiation environments has the potential to benefit NASA missions, the commercial space industry, and other government agencies.To determine the impact of cruise phase vibration on recorded signal quality and use ionizing radiation data to validate results from computer models

Microgravity Investigation for Thin Film Hydroponics (Lily Pond)Space Lab Technologies, LLC

This water- and nutrient-delivery system consists of a plant cultivation system that uses thin-film hydroponic techniques via passive capillary processes to support the growth of nutrient-dense aquatic plants and rooted land plants — a unique space technology that allows a liquid-air interface for aquatic plants.Reliable crop production systems for aquatic plants have enormous potential for edible biomass production in a human habitat on long-duration space missions. Future uses could include food system and life support on crewed NASA missions and the International Space Station.To evaluate the system’s feasibility for operation in microgravity, including its water and nutrient delivery and growth-bed stability

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Learning with NASA

About the PayloadImpact/Potential UsesFlight Test Goals

TechRise payloadsStudent teams across the U.S.

This flight includes 24 student payloads from the first NASA TechRise Student Challenge, which empowers teams of sixth to 12th-grade students to design, build, and launch experiments on NASA-supported test flights.The TechRise Challenge seeks to equip America’s future workforce with the skills needed to advance the U.S. aerospace economy.To give student teams real-world, hands-on experience with the same processes that professional researchers follow

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