A quasi-black hole

Mission

What are we up to?

What our current project entails

Dense matter and compact objects

NEBULA-Xplorer will investigate compact objects such as neutron stars and black hole X-ray binaries within our Milky Way. By investigating these objects, we can learn about fundamental physics such as strong gravity and the equation of state of neutron stars. We can also learn about accretion processes in extreme environments, unable to be reproduced in lab conditions. NEBULA-Xplorer’s coverage of the 0.5-12keV energy range will allow us to observe both the inner-most regions of these systems, where light is most affected by the gravity of compact objects and the magnetic environment of neutron stars.

By observing black holes in this energy range, we can also measure the spin of black holes by observing the relativistic smearing of emission resulting from the illumination of the disk by the corona or by measuring the inner radius of the accretion disk through broad continuum fitting. Understanding the spin population of black holes within X-ray binaries has major implications for stellar evolution in binary systems which are estimated to make up to 85% of star systems in our universe.

Black Hole
Black Hole

Multi-messenger physics

NEBULA-Xplorer frames the multi-wavelength campaigns required to understand jet and accretion physics at the forefront of its design: emphasizing the ability to maximize X-ray observations of time uncertain, fast evolving changes in the accretion flow by tying together fine time resolution of 1 microsecond and the ability to maintain as close to continuous observations of targets as possible.

During longer observations, NEBULA-Xplorer will transmit timing information key to understanding when ballistic jet ejections are launched to the ground to trigger observations from competitive ground-based facilities such as the radio interferometer SKA and mm observatory AMT to maximize the effectiveness of multi-wavelength observations of jets. NEBULA-Xplorer will also work with optical facilities to better understand how activity in the outer accretion disk of these systems propagates into the inner-most regions.

Time-domain Astrophysics

As a non-imaging X-ray timing observatory, NEBULA-Xplorer’s core science focuses on interpreting the variability of emission from the sources that it observes. This includes more traditional ways of thinking about variability such as looking for quasi-periodic signals in source light curve and phase-folded pulse profile modeling of neutron star surfaces but also includes topics such as “dipping” in the light curve produced by clumps of material produced by winds from both the accretion disk and companion star in these systems obscuring the central accretion engine.

Frequently, changes in variability are affected by multiple phenomena in the system that evolve on different time scales, making it difficult to understand how important each phenomenon is to driving transient outbursts or is linked to the fundamental process of accretion. NEBULA-Xplorer’s emphasis on performing continuous longer observations of individual sources will allow us to understand the short-term variability of emission and how that changes on timescales of days to weeks.

NEBULA-Xplorer’s moderate energy resolution and high timing resolution will also allow us to perform spectral-timing analysis of bright systems, like that of the NICER telescope. Spectral timing allows for the investigation of how variability changes with energy, which can be used to trace how the geometry of X-ray sources changes through time as well as understand the distances between different parts of the system through modeling of light travel time within the system.

Black Hole

Mission Goals

Scientific Goal

Better understand how a black hole strips material from an orbiting companion star and how the resulting jets of energy are formed.

Educational Goal

Give students from Dutch educational institutions a first-hand experience of building a space mission from the ground up.

Mission Timeline

Reviews and Design Confirmation

Before production and launch, the project passes formal ECSS review stages. The System Requirements Review (SRR) defines and validates system needs. The Preliminary Design Review (PDR) evaluates the current design. Finally, the Critical Design Review (CDR) confirms readiness for manufacturing and verifies that all requirements are met.

Testing and Qualification (V&V)

Verification and Validation ensures that all systems perform correctly. The Engineering Model (EM) is used for functional testing, while the Proto Flight Model (PFM) undergoes strict qualification tests. Activities include COTS component testing, FPGA prototyping, and alignment of the Optical Bench Assembly to withstand launch conditions.

Assembly, Integration, and Test (AIT)

In the AIT phase, all subsystems are combined into a complete satellite. This includes propulsion and navigation systems such as star trackers. Interface control ensures compatibility between components. The integration of the 15-inch MkII Motorized Lightband connects the satellite securely to the launch vehicle.

Launch Campaign (Pre-launch Phase)

At the launch site, final preparations are completed. The propulsion system is fueled with propylene and nitrous oxide. The satellite is mounted on a SpaceX Falcon 9 as a rideshare payload. The Flight Readiness Review (FRR) confirms launch readiness before liftoff and the start of LEOP.

Rushil Varsnney

Aero Space Engineering, TU Delft

Rushil Varsnney

Aero Space Engineering, TU Delft

The project all corporate projects wish they could be. The place where agile is actually agile. Heed my words, dear reader - this project will serve as valuable experience of the things that can be done right. This was a great experience! Lorem ipsum dolor, sit amet consectetur adipisicing elit. Aspernatur optio maiores quas natus nesciunt ea modi, nihil harum accusantium veniam enim culpa rerum sequi magnam officia. Vero asperiores aspernatur dicta.