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Space Test Program

The Space Test Program (STP) originated from the Space Experiment Support Program (SESP), chartered in 1965 and renamed STP in 1971, as a (DoD) initiative to provide access for DoD-sponsored research, development, test, and evaluation payloads across the military services, enabling the validation of emerging space technologies in orbital environments. Administered by the (SSC) at , , under the leadership of Brian A. Shimek as of 2025, STP operates as a tri-service program with executive management from the . It oversees a portfolio valued at approximately $5 billion, offering end-to-end services including experiment prioritization via the Space Experiments Review Board, mission design, payload integration, launch acquisition on government, commercial, and international vehicles, and on-orbit operations support. Since its inception, the program has facilitated over 600 experiments on more than 300 missions, including dedicated free-flyer satellites, piggyback payloads, flights, and recent integrations, contributing key advancements to systems like GPS and ongoing space warfighting capabilities. Notable historical missions include the 1967 P67-1 launch with and experiments and the 1990 Stacksat (P87-2) multi-payload , while contemporary efforts encompass the 2025 STP-H10 mission delivering six experiments (five DoD, one ) to the ISS and a $237 million awarded to 12 firms for small-satellite development to mature technology.

Overview

Purpose and objectives

The (STP) was chartered in by the Office of the Secretary of Defense to provide dedicated space access for the () research and development () community, enabling the testing of technologies in . The program's primary objective is to maximize the number of experiments flown on available launch opportunities, thereby accelerating the maturation of technologies and reducing overall developmental costs through shared missions and efficient resource utilization. Key goals include demonstrating emerging space technologies in operational environments, validating the performance of systems prior to full-scale deployment, and enhancing space capabilities by bridging the gap between laboratory prototypes and field-ready assets. STP focuses on critical areas such as subsystems for and reliability, sensors for detection and , communications for secure , for maneuverability, and environmental testing to assess durability in space conditions like and microgravity. Evolving from the earlier Space Experiments Support Program established in 1966, STP has facilitated over 620 experiments across more than 280 missions as of 2020, contributing to risk reduction for space initiatives.

Scope of experiments

The Space Test Program (STP) supports a diverse array of experiments focused on advancing Department of Defense (DoD) technologies, encompassing categories such as autonomous systems, radiation effects, propulsion technologies, imaging sensors, communication relays, and space weather monitoring. Autonomous systems experiments evaluate technologies for independent operations, such as the Autonomous Flight Safety System (AFSS) demonstrated on the ORS-3 mission to enhance launch vehicle safety. Radiation effects studies investigate the impact of space environments on electronics and materials, exemplified by the Combined Release and Radiation Effects Satellite (CRRES) which assessed damage to components from radiation belts, and the Demonstration and Science Experiments (DSX) mission that examined artificial radiation belt behaviors. Propulsion technology tests explore efficient in-space maneuvering, including the Long Duration Propulsive ESPA-1 (LDPE-1) for extended operations and the Green Propellant Infusion Mission (GPIM) for alternative fuel systems. Imaging sensors are tested for environmental observation, such as the Lightning Imaging Sensor (LIS) on STP-H5 for global lightning detection and the Compact Ocean Wind Vector Radiometer (COWVR) on STP-H8 for ocean wind measurements. Communication relays advance data transmission, with the Laser Communications Relay Demonstration (LCRD) on STP-3 validating high-speed optical links. Space weather monitoring experiments, like the Solar Wind Interplanetary Measurements (SWIM) and TEMPEST-D on STP-H8, provide data for predicting solar and atmospheric conditions affecting satellites. STP accommodates various payload types to enable flexible experimentation, including dedicated satellites like the STPSat series, which host multiple instruments on single platforms; secondary rideshares that leverage excess capacity on primary launches; CubeSats for compact, low-cost demonstrations; and (ISS) experiments such as those in the Materials International Space Station Experiment (MISSE) series for materials exposure testing. These payload formats allow STP to support both large-scale demonstrations and small, efforts, with CubeSats often deployed via dispensers on missions like STP-S26. ISS-based payloads, managed through the STP-Houston program, integrate external and internal experiments on modules like for extended microgravity testing. The integration approach emphasizes cost-effective access to space, with STP managing end-to-end processes including mission design, payload integration, launch acquisition on vehicles like or , and on-orbit operations to minimize developer burdens. This includes compatibility assessments with host spacecraft and standardization via platforms like the Space Test Experimentation Platform (STEP) for multi-payload missions. Through competitive selection via the Space Experiments Review Board (SERB), STP prioritizes experiments aligned with needs. Notable examples of technology maturation include testing GPS receivers for resilient navigation, the LCRD for maturing laser communications capable of 1.2 Gbps data rates, and demonstrations like the Coupled Ionospheric Research Experiment () on STP-S27 to validate clustering. These efforts transition prototypes to operational use by providing real-world validation. Experiments must adhere to constraints ensuring alignment with DoD priorities, compatibility with host vehicles such as size and power limits, and compliance with safety standards to mitigate risks during integration and launch. Funding typically comes from sponsoring organizations, with STP covering integration costs to enable access.

History

Establishment and early development

The Space Test Program (STP) was chartered in 1965 by the Office of the Secretary of Defense to provide dedicated spaceflight opportunities for Department of Defense (DoD) research and development activities, aiming to consolidate fragmented efforts across military services and reduce duplication in space testing. Initially established as the Space Experiments Support Program (SESP) through a 1966 memorandum from the Director of Defense Research and Engineering, the initiative placed the U.S. Air Force as the executive agent responsible for program management, payload integration, and launch coordination. This structure formalized a DoD-wide approach to leveraging space for military-relevant experiments, with the Air Force's Space and Missile Systems Center overseeing operations from the outset. The program's creation was driven by the intensifying demands of the and the era, where rapid advancements in , , and technologies required reliable orbital testing platforms beyond ad hoc arrangements. The inaugural mission, designated P67-1 and launched on June 29, 1967, from Vandenberg Air Force Base aboard a Thor-Burner II vehicle, marked the program's operational debut with a joint-service : the Navy's Aurora 1 for radiation measurements and the Army's SECOR 9 for geodetic tracking to support applications. Both experiments achieved full success, providing critical data for military databases and demonstrating the viability of multi-service integration on a single launch. Through the late and , STP conducted over 50 experiments, primarily focused on and technologies, utilizing launch vehicles such as the and III to accommodate growing demands. Early challenges included scarce launch opportunities due to competing national priorities and high costs, prompting a strategic shift in the toward multi-payload rideshare configurations to maximize efficiency. A key milestone came in July 1971, when SESP was officially renamed the Space Test Program to reflect its expanded role in testing operational technologies. This evolution culminated in the 1976 launch of LES-8 and LES-9 satellites on an rocket, which successfully demonstrated secure communications for tactical military applications.

Evolution through the decades

In the 1980s, the Space Test Program integrated closely with the , leveraging it as a reusable platform for materials testing and environmental exposure experiments. Starting with in 1982, STP flew 242 experiments across 109 shuttle missions, utilizing Get-Away Special (GAS) canisters and pallet-mounted payloads in the cargo bay to conduct navigation, solar, and environmental data collection. A notable example was the (LDEF), deployed in 1984 and retrieved in 1990, which tested over 10,000 material samples in to assess durability against space hazards. This era emphasized the shuttle's role as a "laboratory in space," driven by a 1978 Department of Defense policy to maximize reusable vehicle capabilities. The marked a pivotal shift following the 1986 disaster, prompting STP to transition from shuttle dependency to expendable launch vehicles for greater reliability and cost efficiency. This adaptation focused on small satellites and innovative deployment methods, with missions like the Space Test Experiments Platform (STEP) series utilizing the for low-cost access to . For instance, the 1990 CRRES mission (P86-1) on an launched a multi-instrument for studies, while the inaugural STEP-1 (P90-1) in 1994 on the first XL flight attempted multi-payload deployment but failed to reach . The decade's emphasis on smallsats aligned with broader goals to streamline space R&D amid budget constraints and post-Cold War priorities. Entering the 2000s and 2010s, STP evolved toward dedicated multi-payload missions, incorporating advanced bus designs and smaller spacecraft to accommodate diverse experiments. The inaugural STP-1 mission in 2007 introduced the EELV Secondary Payload Adapter (ESPA) ring on an rocket, successfully deploying six satellites and marking a new era of rideshare efficiency. This period saw increased integration of NanoSats and CubeSats, as well as deployments from the (ISS), such as the Materials International Space Station Experiment (MISSE) series and Synchronized Position Hold Engage Reorient Evaluate (SPHERES) tests, which evaluated autonomous robotics in microgravity. By this time, STP had launched 88 missions with 157 experiments since 2000, expanding from DoD-exclusive efforts to interagency partnerships, including with for shared ISS access. In the 2020s, STP accelerated its use of commercial launch vehicles to enable agile and responsive space access, reflecting the 2019 establishment of the U.S. and broader DoD reorganization. The STP-2 mission in 2019, launched on a SpaceX , demonstrated this shift by deploying 13 satellites and 12 CubeSats across three orbital planes, showcasing multi-orbit rideshare capabilities. This adaptation responded to the National Space Policy's emphasis on commercial partnerships for cost-effective, rapid launches, including initiatives like the Rapid Agile Launch Initiative (RALI). As of 2024, STP had executed over 300 missions and conducted more than 600 experiments since its inception, with ongoing expansions into interagency collaborations beyond traditional boundaries to address emerging space domain challenges. Recent efforts include the 2025 STP-H5 mission delivering six experiments to the ISS and a $237 million awarded in May 2025 to 12 firms under STEP 2.0 for small-satellite development to mature technologies.

Organization and operations

Management structure

The Space Test Program (STP) is managed as a joint initiative under the of the U.S. Space Force's (SSC), specifically the Advanced Systems and Development Directorate located at , . This structure ensures centralized oversight for coordinating spaceflight opportunities for DoD research, development, test, and evaluation (RDT&E) payloads. Leadership of the STP is provided by a director who serves as the leader, currently Brian A. Shimek as of 2025, heading a team of approximately 63 personnel. The director oversees key functions including mission planning and selection, which is conducted through the Space Experiments Board (SERB), a department-wide panel that annually evaluates and ranks proposed experiments based on criteria such as military relevance, technical quality, and sponsoring agency priorities. This board process begins with service-level reviews and culminates in DoD-level prioritization to allocate limited flight opportunities. Operational processes emphasize efficient integration of STP payloads as secondary rideshares on primary missions, involving coordination with launch providers to match experiment requirements with available orbits and timelines. for these secondary payloads includes rigorous compatibility assessments, environmental testing, and contingency planning to mitigate launch delays or integration challenges while adhering to Air Force Instruction 10-1202 for governance. Primary operations are based at , with additional collaboration from the (AFRL) for technology validation and experiment support. Funding for the STP is provided through DoD RDT&E appropriations, with an annual allocation of approximately $26 million since 2013, supporting the execution of 5-10 missions per year on average to advance maturation. This budget enables the bundling of multiple experiments per mission, optimizing cost-effectiveness for DoD sponsors.

Partnerships and funding

The Space Test Program (STP) maintains extensive partnerships with key entities within the U.S. Department of Defense (DoD), including the (AFRL) and the Naval Research Laboratory (NRL), to develop and test experimental s. These collaborations enable the integration of DoD-sponsored technologies onto shared missions, such as the STP-Houston 9 (STP-H9) effort, which involved AFRL and NRL alongside other labs for payload contributions. STP also partners closely with the National Aeronautics and Space Administration (), leveraging rideshare opportunities on the (ISS) and other platforms to accommodate joint experiments. For instance, collaborates on ISS-based missions like STP-H9, providing launch access and operational support through its ISS Program. Commercial entities play a vital role in STP's launch and spacecraft development, with partnerships including for launch services and for satellite bus construction. 's provided the primary launch vehicle for STP-2 under a contract, demonstrating reusable rocket integration for multi-payload missions. served as the prime spacecraft contractor for STP-3, building the STPSat-6 satellite to host and payloads. Interagency cooperation extends to the (NOAA), exemplified by the inclusion of NOAA's COSMIC-2 payloads on STP-2, a joint effort with Taiwan's National Space Organization to enhance atmospheric data collection. International collaborations are more limited but include contributions through such interagency missions, though direct ties to entities like the (ESA) or remain secondary and focused on data-sharing rather than core payload development. Funding for STP is primarily provided by the through the U.S. Space Force's (), which manages a supporting research, development, test, and evaluation activities. The program covers spacecraft acquisition, integration, launch services, and initial on-orbit operations, drawing from annual budgets to prioritize 40-50 experiments. Shared costs are common for secondary payloads, where partners like contribute funding for their specific technologies, reducing overall expenditure. Integration with the Evolved Expendable Launch Vehicle (EELV) program, now part of the (NSSL) framework, ensures assured access to space by certifying launches for payloads and enabling rideshare opportunities. This model allows to bundle multiple experiments on dedicated or secondary slots, with procuring launch contracts valued in the tens to hundreds of millions, such as the $191 million award for STP-3. Notable examples of shared funding include STP-3, where provided resources for its Laser Communications Relay Demonstration (LCRD) payload through the Technology Demonstration Missions program, complementing contributions for the primary satellite. Similarly, STP-2 benefited from funding for the $165 million launch contract, with partial support from commercial and interagency partners for select payloads. Challenges in STP's partnerships and funding include balancing classified experiments with open scientific payloads from and commercial sources, requiring rigorous risk assessments to avoid interference. Post-2023, funding has shifted toward greater commercial involvement through initiatives like the Space Test Experiments Platform (STEP) 2.0, a $237 million indefinite delivery/indefinite quantity contract awarded in 2025 to 12 vendors, including and others, to procure off-the-shelf spacecraft and reduce development timelines and costs.

Missions

Pre-2000 missions

The Space Test Program (STP), established in 1965, conducted its initial missions starting in 1967, focusing on validating emerging space technologies for Department of Defense applications through secondary payloads on various launch vehicles. Over the pre-2000 era, STP flew approximately 65 missions, accommodating hundreds of experiments that advanced capabilities in satellite communications, , and navigation systems. These efforts laid the groundwork for operational military space assets by demonstrating hardware reliability in orbit. In the and , STP executed more than 20 missions primarily using expendable launch vehicles such as Thor, , Atlas, and , often as secondary payloads alongside primary satellites. A notable example was the 1976 launch of LES-8 and LES-9 on a Titan-3C rocket, which tested secure, jam-resistant communication technologies using relays for transfer between satellites, achieving operational success that informed future systems. Similarly, the 1979 mission, deployed via an Atlas-E launcher, served as a solar observatory while incorporating anti-satellite testing, providing critical data on solar activity's impact on space environments over its multi-year operation. These flights collectively validated reconnaissance and technologies, though documentation remains incomplete for some early efforts. The 1980s marked STP's integration with the , enabling over 10 flights that leveraged the orbiter's payload capacity for diverse experiments, transitioning toward more complex secondary accommodations. The (LDEF), deployed in 1984 aboard (), exposed over 57 experiments—including DoD materials tests—to the space environment for nearly six years, yielding insights into atomic oxygen erosion, radiation effects, and micrometeoroid impacts that enhanced satellite design durability. Following the 1986 accident, STP shifted to expendable vehicles like Atlas and for continued operations. The Combined Release and Radiation Effects Satellite (CRRES), launched in 1990 on an , mapped Earth's radiation belts through chemical releases and particle measurements, confirming models of dynamics that improved navigation and reconnaissance system protections. Overall, these missions advanced understanding of hazards. During the 1990s, STP supported around 15 missions on air-launched rockets and ground-based vehicles, emphasizing cost-effective rideshare opportunities for technology demonstrations. The Space Test Experiments Platform (STEP) series, including STEP 0 through 3 launched between 1994 and 1995 on and , tested advanced sensors, power systems, and attitude control for small satellites, successfully validating in-orbit performance metrics for future operational platforms. The 1999 mission, deployed via Delta-7920, integrated GPS receiver enhancements with imaging payloads, demonstrating precise augmentation that supported applications. Post-Shuttle, expendable launch vehicles dominated, hosting the bulk of flights and roughly 150 experiments across the pre-2000 period, which collectively validated sensors, aids, and tools essential for space operations. Incomplete records persist for cancelled pre-2000 missions, such as P80-1 (Teal Ruby), an sensor demonstration for aircraft detection from that was shelved in the early due to technical and budgetary issues, limiting insights into potential reconnaissance advancements.

2000s missions

The marked a transitional period for the (STP), shifting from reliance on and legacy launchers toward Evolved Expendable Launch Vehicles (EELVs) and multi-payload configurations to accommodate more diverse Department of Defense experiments. This decade saw six major STP missions, emphasizing cost-effective rideshare opportunities and advancements in space weather monitoring, communications, and materials testing. Outcomes included enhanced operational technologies for ionospheric forecasting and polarimetric , with no dedicated STP launches occurring between 2004 and 2006 due to scheduling constraints and integration with other programs. In 2001, STP participated in two key missions. The Space Shuttle flight in August delivered the Materials International Space Station Experiment (MISSE-1 and MISSE-2) to the , where these passive payloads exposed over 800 material samples to the to assess durability against atomic oxygen, ultraviolet radiation, and micrometeoroids, providing critical data for future . Later that year, the Athena I Kodiak Star mission in September achieved the first orbital launch from Alaska's Kodiak Launch Complex, deploying —a student-built satellite with reflective mirrors for laser ranging—and three microsatellites, including payloads for technology validation in . In January 2003, the Coriolis mission launched on a Titan II rocket from Vandenberg Air Force Base, carrying the Windsat polarimetric radiometer for the U.S. Navy to measure ocean surface wind vectors and the Solar Mass Ejection Imager (SMEI) for the to detect solar coronal mass ejections. These instruments demonstrated risk-reduction for the National Polar-orbiting Operational Environmental Satellite System, with Windsat data becoming operationally integrated for . The STP-1 mission in March 2007 represented a milestone as the program's first dedicated EELV flight, launching on an from and deploying six satellites from an ESPA ring adapter: STPSat-1 (hosting ionospheric and auroral experiments), FalconSat-3 (Air Force Academy plasma propulsion tests), MidSTAR-1 (Naval Academy tech demos), the Flight Experiment (radiation-hardened computing), and the Orbital Express pair ( and NextSat-1 for autonomous servicing). This multi-payload approach validated secondary launch capabilities, enabling simultaneous testing of diverse technologies. In April 2008, the Communications/Navigation Outage Forecasting System (C/NOFS) launched on a Pegasus XL rocket from , carrying six instruments to study equatorial ionospheric bubbles and forecast effects on GPS and communications. Operating in a low-inclination , C/NOFS provided real-time data that improved models for signal degradation in the .

2010s missions

The marked a period of expansion for the Space Test Program (STP), emphasizing rideshare opportunities on small and medium launch vehicles, as well as the deployment of dedicated STPSat platforms to host multiple experiments. This decade saw STP leverage both government-provided rockets like the series and emerging commercial options, including vehicles, to fly over a dozen payloads focused on technology maturation in areas such as sensor phenomenology, space weather , and autonomous systems. These missions advanced DoD capabilities by demonstrating cost-effective to space for risk-reduction experiments, with a total of five key launches enabling the integration of CubeSats and standardized interfaces. In November 2010, STP-S26 launched aboard a rocket from Kodiak Launch Complex in , marking the program's 26th small-launch mission. The primary payload, STPSat-2—built by Aerospace as the first Standardized Interface Vehicle ()—hosted three experiments: two Space Phenomenology Experiment (SPEX) units to assess performance in the and the Ocean Data Telemetry Microsat (ODTML) for two-way . Additional secondary payloads included FASTRAC formation-flying satellites, FASTSAT with the NanoSail-D demonstrator, FalconSat-5 for propulsion tech, O/OREOS for microbial survival studies, and RAX for ionospheric research. All payloads were successfully deployed to a 650 km , with STPSat-2 operating for over a year to validate modularity for future multi-payload flights. The November 2013 ORS-3 mission, utilizing an Orbital Sciences I from , , featured STPSat-3 as its primary spacecraft alongside 28 s. STPSat-3 carried six experiments, including the Autonomous Flight Safety System (AFSS) demonstration for real-time on responsive launches, and the Integrated Miniaturized Electrostatic Analyzer - Recomputed (iMESA-R) for space weather plasma measurements by the U.S. Academy. Other payloads encompassed the Joint CubeSat Operations and Research Experiment () for command-and-control tech, Tactical Communications Experiment (TCTE) for laser communications, and Sensors for Strategic U.S. Unspecified (SSU) and Space Weather Atmospheric and Technology Sensor (SWATS) for . The mission successfully validated rapid-integration processes, with AFSS enabling autonomous trajectory termination and iMESA-R collecting ion data over its one-year lifespan in . In 2014, STP facilitated the deployment of the Naval Research Laboratory's SpinSat from the via NASA's Cyclops system, launched initially aboard Cygnus CRS-4 on an rocket in September. SpinSat, a 10 kg sphere with a deployable tether and solid-propellant microthrusters, tested attitude control and deorbit technologies in after release in November. The mission demonstrated scalable propulsion for small satellites, operating until early 2015 and providing data on thruster performance under microgravity conditions. The decade's largest STP effort came in June 2019 with the STP-2 mission on a Falcon Heavy from , , deploying 24 satellites across multiple orbits to certify the vehicle for use. Key payloads included six COSMIC-2 satellites for global navigation satellite system to study weather and climate, the Deep Space Atomic Clock for precision navigation, and 18 CubeSats such as the Planetary Society's LightSail 2, which successfully demonstrated controlled sailing by raising its orbit using sunlight pressure alone. The mission achieved all objectives, including complex multi-plane insertions, and advanced propulsion concepts with LightSail 2 operating until 2022. Later that year, in November 2019, STPSat-4 launched on Northrop Grumman Cygnus NG-12 via from Wallops, with deployment from the ISS in January 2020. STPSat-4 hosted experiments in communications and power systems but experienced a partial array failure; it reentered and decayed in October 2022 after completing its objectives. Overall, these five missions utilized a mix of government (, ) and commercial (, /Cygnus) vehicles, flying diverse payloads that advanced autonomous operations through AFSS and solar sailing via . While successful, gaps remain, including incomplete manifests for secondary payloads on some flights. STPSat-5 was launched in December 2018 on the SSO-A rideshare mission via Falcon 9.

2020s missions

The 2020s marked a shift in the Space Test Program (STP) toward greater integration with commercial launch providers and rideshare opportunities, enabling more frequent and cost-effective testing of amid evolving needs. By 2023, STP had executed at least three dedicated missions, leveraging vehicles like the and for primary and secondary payloads focused on communications, propulsion, and environmental monitoring. These efforts validated key capabilities, such as laser communications and tactical data links, while highlighting challenges like launch failures in deployments. Ongoing activities emphasized secondary integrations on (NSSL) missions and (ISS) experiments, with no major dedicated STP flights reported in 2024 but one in 2025. In December 2021, the STP-3 mission launched aboard a 551 rocket from , successfully deploying the primary spacecraft STPSat-6 and seven secondary payloads into geosynchronous transfer orbit. STPSat-6 hosted nine experiments, including the Space and Atmospheric Burst Reporting System-3 (SABRS-3) from the for nuclear detonation detection and NASA's Laser Communications Relay Demonstration (LCRD), which achieved bidirectional data transmission rates up to 1.2 Gbps, demonstrating high-speed optical communications for future missions. Among the secondaries, the Long Duration Propulsive Evolved Expendable Secondary Payload-1 (LDPE-1)—a ring-shaped —tested extended propulsion in geosynchronous orbit, enabling over 500 days of operations and paving the way for standardized rideshare architectures. The mission's outcomes advanced risk reduction for space systems, with LCRD operational data contributing to NASA's broader optical networking goals. The STP-S27 mission in January 2023 attempted to deploy payloads via Virgin Orbit's air-launched rocket from Spaceport , , but failed to reach orbit due to a second-stage anomaly, resulting in the loss of all satellites. Intended for , the mission carried the Coordinated Ionospheric Reconstruction Experiment (CIRCE) 1 and 2 CubeSats, a joint U.S.-U.K. effort to study ionospheric dynamics using multi-sensor measurements for improved forecasting, and the 2A and 2B 6U CubeSats for testing radio signal monitoring, including GPS and imaging technologies. Despite the failure, the integration process highlighted STP's international partnerships and the potential of responsive small-launch capabilities for tactical experiments. No orbital data was obtained, underscoring risks in emerging commercial launchers. Later in June 2023, the STP-CR2301 rideshare mission successfully launched three CubeSats aboard SpaceX's Transporter-8 from , delivering them to sun-synchronous as part of a 72-payload manifest. The payloads included Modular Intelligence, Surveillance, and Reconnaissance (MISR)-A and -B, which tested scalable, modular sensor architectures for rapid deployment in intelligence gathering, and XVI, which validated space-based extensions of the Link-16 network for secure, real-time communications between air, sea, and space assets. These experiments demonstrated commercially available bus platforms' viability for needs, with XVI achieving initial Link-16 transmissions to ground stations, enhancing . From 2024 to mid-, STP focused on secondary payloads integrated into NSSL and commercial rideshares, with no standalone dedicated missions reported. In July , the STP-28C mission deployed the Athena spacecraft—a collaborative NASA-DoD —aboard a from Vandenberg, testing scalable satellite technologies for quicker launches and orbital demonstrations of instruments. Ongoing ISS-based activities, such as the STP-Houston series (e.g., STP-H10 in ), continued external payload exposures for materials testing and technology maturation in microgravity. STP-H10, launched in April aboard CRS-32, delivered six experiments to the ISS for external exposure on the module. As of November , future plans include the STP-S29A mission with STPSat-7 aboard a , targeted for late , to host advanced experiments like AI-driven satellite health prediction and orbital debris detection.
MissionLaunch DateVehicleKey Outcomes
STP-3Dec 7, 2021Laser comms validation (1.2 Gbps); propulsion endurance (>500 days)
STP-S27Jan 9, 2023 (failed)No orbital data; integration success for and signal monitoring tests
STP-CR2301Jun 12, 2023Link-16 space extension; modular sensor demos
STP-28CJul 22, 2025Scalable sensor deployment; initiation

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