Digital Commons Network^™

Veery, A Flat Satellite Scatterometer For Global, Hourly Refresh Of Ocean Surface Vector Winds, M. Patrick Walton, Alex R. Laraway, David G. Long

Small Satellite Conference

Care Weather is developing Veery, a small satellite scatterometer for monitoring ocean surface vector wind (OSVW) with state-of-the-art performance. Veery uses a rotating fan-beam C-band radar to provide a 1,050 km swath with 25 km resolution and more than 70% uptime. Veery’s dynamic range covers 3–27 m/s with speed errors below 1.6 m/s and directional errors below 11^°, matching the performance of previous scatterometers from a much smaller satellite. Veery’s small size is enabled by a flat satellite form factor that vertically integrates the instrument and bus. That small size makes it affordable for deployment in a constellation …

Innocube – First In-Orbit Results Of The Fully Wireless Satellite Data Bus, Tom Baumann, Erik Dilger, Sergio Montenegro, Felix Sittner, Moritz Arbab, Thomas Walter

Small Satellite Conference

The Innovative CubeSat for Education (InnoCube) mission is a technology demonstration CubeSat that relies entirely on a wireless data bus for intra satellite communication. It was launched in January 2025 onboard SpaceX Transporter-12. This paper presents the mission objectives and initial results, with a particular focus on the performance and reliability of the wireless system.

InnoCube is a collaborative project between the University of Wuerzburg and Technische Universität Berlin in Germany. Its primary objectives are to demonstrate the feasibility of a fully wireless data bus for intra-satellite communication, provide a testbed for new technologies, and offer students hands-on experience in …

The Auroral X-Ray Imager (Axis), Andrew Holland, Karen Holland, David Colebrook, Thomas Buggey, Chiaki Crews, Michael Hubbard, Colin Forsyth, William Dunn, Shyama Narendranath, Srikar Tadepalli, Anurag Tyagi, Koushal Vadodariya, Douglas Jordan

Small Satellite Conference

The interaction of the solar wind with the Earth is a subject of significant study. One phenomenon is the occurrence of aurorae at the polar regions, resulting from the interaction of particles in the solar wind with the atmosphere, often giving light shows which captures the publics’ imagination. These energetic interactions also extend to X-ray wavelengths. Whilst aurorae have been studied for generations in the visible, the X-ray emission of aurorae has only been observed by a couple of spacecraft, with a paucity of data. There are only a couple of instances of emission intensity having been measured, but without …

Seeing 230 Ident: A Compact, High-Precision Zerodur®-Based Imager For Smallsat, A. Bouée, X. Bozec, J. L. Carel, F. Dong, V. Dumont, L. Duveau, P. Manfredi, V. Mengeling, R. Philipps, S. Ques, C. Soncin, L. Swyngedauw

Small Satellite Conference

The SEEING 230 IDENT is a compact space imager based on a ZERODUR^® main structure. It provides a ground sampling distance of 1 meter when operating at an altitude of 500 km. The optical layout adopts a space-efficient Korsch design, optimized for compactness and performance. This paper provides a comprehensive presentation of the instrument’s main specifications, its opto-mechanical concept, and the experimentally validated performance.

Ninjasat Achievements And Lessons Learned, Toru Tamagawa, Takao Kitaguchi, Yo Kato, Tatehiro Mihara, Kentaro Taniguchi, Teruaki Enoto, Tomoshi Takeda, Hiromitsu Takahashi, Naoyuki Ota, Amira Aoyama, Satoko Iwata, Takuya Takahashi, Kaede Yamasaki, Yousuke Nakano, Soma Tsuchiya, Yuto Yoshida, Syoki Hayashi, Sota Watanabe, Arata Jujo, Yuanhui Zhou, Keisuke Uchiyama, Wataru Iwakiri, Mayu Ichibakase, Masaki Numazawa, Hiroki Sato, Chin-Ping Hu, Hirokazu Odaka, Tsubasa Tamba

Small Satellite Conference

NinjaSat is a 6U CubeSat dedicated to X-ray astrophysics, launched on November 11, 2023. Scientific observations began on February 23, 2024, and as of June 27, 30 X-ray sources have been observed, yielding numerous scientific outputs. Beyond its primary mission of astronomical observations, NinjaSat has contributed to additional fields, including X-ray pulsar-based navigation, atmospheric studies using X-rays passing through Earth’s limb, investigations of atmospheric structure through orbital decay analysis, and studies of the relationship between the orbital radiation environment and solar activity. By expanding beyond its initial astronomical focus, NinjaSat has demonstrated the versatile potential of scientific CubeSats. This paper …

Climate - Commercial And Scientific Instrument Opportunities For Small Satellite Constellations, Alex Da Silva Curiel, Rob Elliott, Tony Canas, Stephanie Mottershead, Andy Palfreyman, Martin Sweeting Sir

Small Satellite Conference

There is an economic and social impact in many areas in the world due to lack of information on local climate, and better understanding is widely believed to lead to cost savings and improved living standards. Despite the wealth of spacecraft data available today, many climate variables are still poorly monitored. Small satellites in constellation can help in filling data gaps, and also provides the important temporal resolution required. Such missions could be highly complementary to the NASA NEO and EU Copernicus programs, and their data can be commercially valuable, opening up the potential for novel business models and services. …

Launch Fast Learn Fast: Lessons Learned From The R5-S2 And R5-S4 Missions, James Berck, Sam Pedrotty, Jack Wisbiski, Morgan Alexander, Kathryn Knesek, Ruth May, Jacob Nunez-Kearny, Rob Stoddard, Thomas Kirven, Robin Onsay, Roger Hunter

Small Satellite Conference

The Realizing Rapid, Reduced-cost high-Risk Research (R5) project is pushing the envelope on minimizing cost and schedule for complex spacecraft that support low Technology Readiness Level payload demonstration in Low Earth Orbit (LEO). R5 has recently designed, built, launched, and operated multiple spacecraft that are iteratively and incrementally delivering improved payload hosting capabilities while maintaining cost targets (< $100k in materials per bus) and schedule targets (launching at least two spacecraft per year). This paper will describe the unique architecture, approach, technological advancements, and lessons learned from the project. The primary stakeholder for R5 is the Small Spacecraft Technology program within the Space Technology Mission Directorate at NASA with the project based out of Johnson Space Center.

To achieve the aggressive cost and schedule targets, R5 is redefining the understanding of how much rigor, quality, and robustness are required to succeed in high-risk LEO missions. Starting with a clean-slate for process and system design, R5 has charted a path, …

Pushing The Boundaries With The Thinsat And Troop Platforms: Flight Results Of Recent Launches Testing New Systems, Matt Orvis, John Pugsley, Nathan Turner

Small Satellite Conference

Flash Talk presented during the 2025 SmallSat Conference.

Development Of Turbopump For Zero Rocket Engine, Hiroshi Tomaru, Shinnosuke Yabuki, Shota Yamanaka, Ryosuke Tomiyama

Small Satellite Conference

Flash Talk presented during the 2025 SmallSat Conference.

Using Capstone’S Mission Extension To Navigate The Future Of Cislunar Technology, Alec Forsman, Michael Caudill, Anthony Zara, Matthew Givens, Rebecca Rogers, Lauren De Moudt, Ethan Kayser, Thomas Gardner

Small Satellite Conference

Launched in late June 2022, the Cislunar Autonomous Position System Technology, Operations, and Navigation Experiment (CAPSTONE) has been operating in the Earth-Moon, Southern L2 Near Rectilinear Halo Orbit (NRHO) for more than two years. After successfully completing its primary mission objectives, CAPSTONE was awarded a 15-month mission extension in September of 2024. The goal of this extension was to continue to use CAPSTONE to provide valuable and informative data to the NASA Gateway program and leverage the platform to raise the TRL of several cislunar technologies. This paper presents a detailed analysis of the operational data obtained throughout the mission, …

Expanding Cubesat Horizons: A 27u Mission To Sun-Earth L5, Tabitha Patrick, Allen Martinez, Aimee Dew, Shane Hancock, Michael Generale

Small Satellite Conference

CubeSats have gained increasing popularity in the aerospace industry due to their compact, modular designs, which offer a cost-effective and versatile solution for orbital applications. Historically limited to low Earth orbit (LEO) due to propulsion and communication constraints, CubeSats are now being explored for deeper space missions. The Icarus mission seeks to demonstrate that a 27U CubeSat can operate at the Sun–Earth Lagrange Point 5 (L5), leveraging recent advancements in efficient electric propulsion and deployable subsystems to monitor solar activity and relay data back to Earth. By capitalizing on a standardized CubeSat form factor with commercial off-the-shelf components, Icarus offers …

Sardonyx: A Building Block Towards In-Space Assembly, Michael Swartwout

Small Satellite Conference

In-space assembly and manufacturing (ISAM) is an enabling capability for future space missions, and one where small satellites can play an essential role. Of the many technologies needed for ISAM, the Sardonyx mission will demonstrate two: capture of noncooperative resident space objects and close-proximity, agile maneuvering. Sardonyx is a partnership between Saint Louis University, Cambrian Works and Bennett Research Technologies.

The baseline design consists of a single 12U-scale spacecraft carrying multiple deployable Objectives. Each Objective will expand to at least a meter in diameter and be gently released. The Sardonyx spacecraft will detect the target, maneuver to within a few …

Debrisfind: A Cubesat Mission For Evaluating Space Debris Flux In Low Earth Orbit, Ishriak Ahmed, Imraan A. Faruque

Small Satellite Conference

Proliferation in low earth orbits, both operational satellites and defunct or debris items, poses a significant challenge to the long-term sustainability of space operations, and the difficulties in tracking and measuring mm-scale has increased the uncertainty of contemporary statistical models like the NASA Orbital Debris Engineering Model (ORDEM) and ESA MASTER and their statistical debris flux predictions. This uncertainty both complicates orbital mission risk assessment and impedes remediation efforts. This paper develops a CubeSat mission that informs these statistical models through in situ flux determination, providing a comparison of debris flux levels in Low Earth Orbit (LEO). The optimum orbit …

Development Of Model Predictive Control Approach For Precise De-Orbit Of Nanosatellite Using Aerodynamic Drag, Tian Xie, Takashige Suzuki, Maximilien Berthet

Small Satellite Conference

Small satellite missions in low Earth orbit (LEO) can utilize propellant-free aerodynamic drag for maneuvering, but achieving precise orbit control is challenged by non-linearities and uncertainties. This paper proposes a nonlinear model predictive control (NMPC) framework designed for precise trajectory tracking under these conditions. By focusing on following a given reference path, our NMPC controller overcomes time-varying perturbations (e.g., J2, J3, J4 effects). We validated this tracking-focused approach with simulations incorporating stochastic atmospheric models. Monte Carlo analysis, using controlled de-orbiting profiles as reference trajectories, demonstrates that our NMPC system provides a powerful tool for enabling precise, propellant-free maneuvers. This work …

Review Of Microgravity Biotechnology For Space Applications: The Anujiva Perspective, Saranya Ravva, Yukti Makkar, Abeneth Ramachandran, Sai Kiran Parre

Small Satellite Conference

Biomanufacturing in microgravity presents transformative opportunities for biotechnology beyond the limitations of terrestrial environments. Gravity-driven convection, sedimentation, and contamination risks often hinder biological productivity on Earth. In contrast, space-based conditions enhance protein crystallization, three-dimensional cell culture, and the production of novel biomaterials. This review synthesizes recent advancements in microgravity-enabled biotechnology, drawing from recent peer-reviewed literature and mission data.

We focus on the emerging field of autonomous bioreactor systems for space applications, emphasizing innovations in miniaturization, closed-loop environmental control, and real-time sensing. As a representative case study, we examine the AnuJIVA initiative, a CubeSat-based platform engineered for cultivating microorganisms such as …

Outer Planet Exploration By Novel And Small Spacecraft: Jaxa’S Opens Program Concept And Its First Mission Opens-0, Ryu Funase, Naoya Ozaki, Hajime Yano, Isas/Jaxa Opens Working Group

Small Satellite Conference

The OPENS (Outer Planet Exploration by Novel Small spacecraft) program, proposed by JAXA's Institute of Space and Astronautical Science (ISAS), aims to revolutionize outer planet exploration through the use of small, low-cost spacecraft. Unlike traditional flagship-class missions, OPENS promotes high-frequency, high-risk, high-return missions that can be achieved even by countries with limited resources. The program’s first mission, OPENS-0, targets the demonstration of key technologies necessary for future small outer planet explorers, including solar-powered spacecraft operations and long-term hibernation capability. The spacecraft will be launched by JAXA’s Epsilon S rocket and perform gravity assists en route to Saturn, with the earliest …

High Resolution, Wide Swath Sar Observation From Disksat At Vleo, Hirobumi Saito, Yasuyuki Miyazaki, Michio Takikawa, Tien M. Nguyen, Roy Nakagawa, Ching-Yao (Tony) Chang, David Hinkley, Ryo Natsuaki, Mitsuteru Kaneoka, Jiro Hirokawa, Kazuyuki Nakamura

Small Satellite Conference

This paper proposes a novel concept of quasi-two-dimensional SAR (synthetic aperture radar) satellites, SAR DiskSats, featuring a deployable passive slot array antenna (De-PSAA) that can be compactly folded within the quasi-two-dimensional (Q-2D) satellite body. This Q-2D configuration allows for potential flexible solar cell sheets to be installed on the backside of the antenna, as the antennas do not dissipate heat. This satellite configuration is also suitable for stacking within a rocket fairing for the mega-constellation launch of SAR DiskSats into VLEO (very low Earth orbit). The proposed DiskSat's thin edge cross-section reduces aerodynamic drag, enabling the satellite to operate at …

Astra – Autonomous Satellite Technology For Resilient Applications: A Technology Demonstrator, Lauren Underwood, Fernando Figueroa, Zachary Lewton, Landon Tynes, Travis Martin, Jonathan Morris, Quentin Oswald, John Curry

Small Satellite Conference

ASTRA is an on-orbit technology demonstrator establishing a new paradigm for implementing on-board “thinking.” ASTRA is a system-level autonomy capability (including digital twins, anomaly detection, diagnostics/prognostics, and mission management) enabled by an innovative technology, NPAS - NASA Platform for Autonomous Systems. NPAS is developed by NASA Stennis Space Center (SSC) Autonomous Systems Laboratory (ASL) with support from NASA Exploration Systems Development Mission Directorate (ESDMD) Advanced Exploration Systems and Mars Campaign Office. ASTRA leverages NPAS for on-board “thinking” autonomy. ASTRA also includes advanced hardware required for implementing autonomy. ASTRA Flight Software (FS) is running on commercial hardware that provides the computational …

Kentucky Re-Entry Probe Experiment-3: The Third Hypersonic Flight Of The Krups Capsules, Bruno Tacchi, Eric T. Adams, Alexander R. Barrera, Asa C. O'Neal, Aaron Cramer, James E. Lumpp, Savio J. Poovathingal, Alexandre Martin

Small Satellite Conference

The Kentucky Re-entry Universal Payload System (KRUPS) is a small flight capsule with dimensions of 11 by 8.5 inches and a sphere-cone geometry. KRUPS aims to serve as a cost-effective testbed for hypersonic atmospheric entry experiments, collecting thermal response and flight data during re-entry and testing novel thermal protection systems (TPS). The forebody of the capsule is fitted with an instrumented TPS containing thermocouples and pressure ports. Furthermore, the instrumentation suite contains a high-g accelerometer, a GPS, an IMU, and a spectrometer.

The KRUPS project started in 2013. Since then, the capsule has flown five sounding rocket missions, a high-altitude …

On-Orbit Validation Of An Ai-Enabled Cloud Removal And Compression Solution For Eo Satellites, Rosana Rodríguez-Bobada, Jose Manuel Heredia-Oliver, Pablo Tomás Toledano González, Carlos Espinosa-Peral, José Luis Espinosa-Aranda, Tom Hendrix, Amaury Perrocheau, David Rijlaarsdam, Aubrey Dunne

Small Satellite Conference

Optical Earth Observation (EO) sensors can be significantly affected by atmospheric conditions, particularly cloud cover, which can obscure their images and reduce the information content in the final image. It is estimated that over 50% of the Earth’s surface is covered by clouds at any given moment. As a result, up to half of the data captured by visible EO satellite imagers is rendered unusable for most applications. Transmitting this unusable data, even in a compressed form, unnecessarily utilises valuable communications downlink bandwidth. This is particularly acute for hyperspectral EO missions, where the tens to hundreds of bands per acquisition …

Novel Global Navigation Satellite System Receiver For Characterization Of Ionospheric Scintillation And Plasma Bubbles With A Cubesat Swarm, William Gullotta, John Braun, Jan-Peter Weiss, Nicholas Pedatella, Qian Wu

Small Satellite Conference

Ionospheric scintillation and equatorial plasma bubbles (EPBs) are phenomena related to turbulence and depletion in the plasmas in the ionosphere. EPBs are depletions in the plasma density in the equatorial region in the post-sunset period. These depletions can lead to turbulent irregularities in the amplitude and phase of communications signals, called scintillation. Scintillation also occurs in the polar regions, where it is caused by particle precipitation and convection. EPBs and scintillation in low- and high- latitudes both have an impact on the quality and availability of space-based communication and navigation systems which leads to a high demand for observations from …

Advancing Space Weather Research With The Next-Generation Space Weather Probes, Justin Wellington, Rowan Antonuccio, Kade Howes, Benjamin Lewis, Todd Wilson, Charles Swenson

Small Satellite Conference

Accurate characterization of ionospheric conditions is essential for improving space weather forecasting and mitigating its impacts on communication, navigation, and space-based systems. Utah State University’s Center for Space Engineering has developed the second-generation Space Weather Probes (SWP2) instrumentation suite, optimized for deployment on small satellite platforms. Building upon experience from the Scintillation Prediction Observations Research Task (SPORT) mission, SWP2 integrates advanced Langmuir probes, floating potential double probes, and an RF impedance probe onto a compact, FPGA-controlled electronics module, conforming to the standard 9×9 cm CubeSat form factor. The design provides complementary diagnostic measurements of electron density, electron temperature, electric fields, …

Slalom: A Mission Concept For Autonomous Very Low Lunar Orbit Operations, Jeffrey S. Parker, Bradley Cheetham, Charles Cain, Ethan Kayser

Small Satellite Conference

A Sustained Low-Altitude Lunar Orbital Mission (SLALOM) maintains an orbital path very close to the surface of the Moon: passing within 1–5 kilometers of topographical peaks and maintaining an average altitude under 10 kilometers. This extremely low orbit enables high-resolution observations of the Moon but requires a new class of autonomous navigation and stationkeeping. The au-tonomous software system, ALPINE (Auto-maneuver Location Processor using Integrated Navigation Estimates), fuses real-time optical navigation data with one-way and cross-link radiometric tracking data to maintain continuous and autonomous custody of the spacecraft. This paper examines a stationkeeping strategy that maximizes surface coverage of desirable locations …

Chipsat Design For The Descent Mission, Matt Hurford, Bryan Peters, Joshua Umansky-Castro, Corbin Heywood, Andy Filo, Alex Burke

Small Satellite Conference

The Demonstration of Suborbital ChipSats Ejected from New Shepard Test Flight (DeSCENT) mission, conducted by Cornell’s Space Systems Design Studio (SSDS) in partnership with the Applied Physics Laboratory (APL), is a suborbital endeavor that aims to deploy 100 ChipSats from a Blue Origin New Shepard rocket when the rocket reaches 100 km above the Earth’s surface. ChipSats are a type of FemtoSat (satellite with a mass less than 100 grams) that can fit into the palm of your hand and contain all the fundamental functionality of a spacecraft. The mission’s primary objective is to refine models that predict the freefall …

Productization And Qualification Of A 22n Bipropellant Hydrogen Peroxide Engine, Thomas White, Vivek Vidyarthi, Avery Clotfelter

Small Satellite Conference

As the space industry expands quickly and green propellants enjoy growing interest, the key question of research is no longer basic viability but productization. The most valuable engine is one that is qualified and available as close to “off the shelf” as possible. But publications on the process of taking an engine from first demonstrations to true product status are rare. This paper describes the process of transitioning Benchmark Space System’s 22N Ocelot engine – first flown as the 1.0 product version in 2022 – into a high-volume, well-characterized product, including details on the qualification program for the 1.2 version, …

Designing Coordinated Multi-Vehicle Networks For Leo-To-Geo Transport Using Low-Thrust Propulsion, Shan Selvamurugan, E. Glenn Lightsey

Small Satellite Conference

Elements of on-orbit servicing (OOS), such as propellant depots and refuellable servicing spacecraft (servicers), offer promising means to extend the operational lifespan of Earth-orbiting assets. While current concepts for reusable in-space transportation often rely on a single, versatile servicer to transfer payload satellites to high-energy orbits, an alternative approach to this monolithic architecture may employ a network of space-resident transport vehicles to move payloads from low-Earth orbit (LEO) to geostationary orbit (GEO). This paper investigates how servicers equipped with low-thrust propulsion can be used to design fuel-optimal, multi-vehicle transport architectures under temporal constraints. A set of analytical solutions is derived …

Leopard: Demonstrating Cubesat Technologies For Light Scattering Observations And Satellite Positioning In Leo For Future University-Based Lunar Missions, Necmi Cihan Orger, Victor Hugo Schulz, Jose Rodrigo Corodova-Alarcon, Hanadi Abdalla, Mehmet Esit, Makiko Kishimoto, Sara Aziz, Mengu Cho, Minh Pham Anh, Hery Steven Mindaro, Subsinchai Ratatamanun, Enkhmend Ochirsukh, Husseinat Etti-Balogun, Kubo Shota, Jeje Kudakwashe, Thibaut Tena, Rafiki Yves Ndayishimiye, Daisuke Nakayama, Alper Sanli, Konosuke Nishinaga, Akihiro Oboshi, Edgar Mujuni, Ramson Munyaradgi Nyamakondiwa, Im Polimey, Hiroto Hidaka, Hirokazu Masui, Josue Reynel Galindo Rosales

Small Satellite Conference

The LEOPARD (Light intensity Experiment with On-orbit Positioning and satellite Ranging Demonstration) satellite is a 3-unit (3U) CubeSat platform to demonstrate several technologies and payloads in low Earth orbit (LEO) prior to future lunar CubeSat missions. After deployment from the International Space Station (ISS), it plans to perform the following missions, including onboard processing of Earth-origin one-way radio ranging signals (OPERA), multispectral imaging to monitor light scattering above the horizon (MSC), single event latch-up detection (SEL), solar panel deployment using shape memory alloy (SMA), and ambient magnetic field measurements. First, the OPERA mission will validate critical steps towards deep-space positioning …

In 8 Years From Design To Launch: Objectives, Challenges And Risk Mitigation Of The Educational Student Cubesat Project Source, Philipp Hoffmann, Kaja Gebhard, Mario Spahr, Klemens Boltenhagen, Michael O'Donohue, Daniel Galla, Robin Schweigert, Natascha Bonidis, Sabine Klinkner

Small Satellite Conference

The Stuttgart Operated University Research CubeSat for Evaluation and Education (SOURCE) project is a 3U+ CubeSat developed in collaboration between the Small Satellite Student Society at the University of Stuttgart (KSat e.V.) and the University of Stuttgart’s Institute of Space Systems. This educational satellite mission is designed to provide students with hands-on experience in all phases of satellite development, from the initial concept to the final mission operations. SOURCE’s development began in 2018 and has been supported by ESA’s Fly Your Satellite! program since 2020. Over the past seven years, more than 500 students have had the opportunity to work …

High-Performance Green Hydrazine-Based Propellant For Small Spacecraft, Robert K. Masse, Andrew R. Haviland, Benjamin A. Glassy, Ronald A. Spores, Joshua L. Rovey

Small Satellite Conference

Whereas the last decade has seen a notable expansion in the number of small spacecraft on orbit, a lack of high-total-impulse chemical propulsion options continues to hamper their complete proliferation into mission arenas requiring dynamic maneuvering. This has been particularly true at the NanoSat/CubeSat scale, where volume limitations are most constraining. Because SmallSats are generally launched as secondary payloads, green ionic liquid propellants such as ASCENT and LMP-103S have been recognized as particularly advantageous in that they introduce minimal logistical impacts to primary payload integration workflow. However, despite the substantial packaging advantages conferred by their high impulse density, these propellants …

Game-Changing Technologies For Green Propulsion Operating With 98% Hydrogen Peroxide, Pawel Surmacz, Adrian Parzybut, Michal Ranachowski, Zbigniew Gut, Michal Alaszkiewicz

Small Satellite Conference

The propellant grade hydrogen peroxide is coming back to space industry. While launcher applications would accept lower grades of High Test Peroxide (HTP) for cost reduction, the highest possible concentration matters much more for in-space propulsion. Every 1% in peroxide concentration translates to the propulsive performance (specific impulse) roughly in 1% for monopropellant and 0.5% for bipropellant.

The highest HTP grade provides certain advantages. While being more reactive, it requires less catalyst for its full decomposition, resulting in hardware mass and cost reduction. When used with any kind of bipropellant (either catalyst-augmented or hypergolic, and including hybrid), the highest grade …