NUSOL MISSION   

Measurement of solar neutrinos is important for scientific studies aimed at understanding the interior
of the Sun. While there have been many Earth-based experiments measuring solar neutrinos, one has never been done in space. Around 2015, Dr. Nick Solomey of 蹤獲扦 Physics envisioned flying a small-sized neutrino detector close to the Sun. Since then, there has been an increasing interest within NASA to conduct scientific studies in space using a neutrino detector. Formally referred to as the NuSol, the mission idea is centered around the fact that high solar neutrino flux close to the Sun only makes a small-sized detector necessary for the experiments. Detectors used for Earth-based studies are typically very large, of the order of 10,000 kg, and a detector flying close to the Sun (Parker Solar Probe distances) will allow for two orders of magnitude reduction in the detector size. In addition, a space-based study has additional advantages. For instance, Earth-based detectors lie deep underground and the neutrinos interacting with them have many sources: Sun, cosmic rays, and terrestrial nuclear experiments; hence, any Earth-based study needs to be able to separate the effect of cosmic rays and geoneutrino sources in order to be able to relate the experimental results to processes happening at the Sun. In contrast, a detector approaching the Sun on a spacecraft will see a decreased flux of cosmic rays and geoneutrino sources are absent; hence, the experimental results will be directly correlated to the solar processes. Furthermore, there are unique scientific phenomenon related to the transition of coherence of solar neutrinos that happen near the Sun, and can never be observed by an Earth-based study. To this end, the NuSol mission study, supported by the NASA Innovative Advanced Concepts (NIAC) program, investigated the feasibility of a scientific demonstration mission for in-space solar neutrino detection; it was observed that flying a detector on a probe flying the trajectories similar to that of Parker Solar Probe would be a practical solution that allows for sufficient scientific studies and yet keep costs reasonable owing to reuse of spacecraft bus components that have flight heritage from
Parker Solar Probe mission. 

SNAPPY MISSION    

Recognizing the fact that a solar neutrino detector has never flown in space, the Phase-III part of
the NIAC project focuses on the development of a CubeSat to validate the operation of a prototype
detector in near-Earth space. It is important to note here that in near-Earth environment, a smallsized
CubeSat-class detector will not be able to detect any solar neutrino. However, the CubeSat
mission provides opportunities to validate the detector with respect to its interaction with cosmic
rays (background). The 3U CubeSat is anticipated to be launched in 2025 into a sun-synchronous low-Earth orbit and will gather scientific data primarily over the poles (both North and South poles). 

PUBLICATIONS

2021 AAS/AIAA Space Flight Meeting 

Preliminary Mission Design for Proposed NuSol Probe 

Authors: K. Messick, A. Dutta, H. Meyer, M. Christl, N. Solomey 

Abstract: A solar neutrino detector has never flown in space. NuSol is a proposed mission
to fly a solar neutrino detector close to the Sun in order to conduct unique sci-
ence objectives that cannot be realized by detectors on Earth. The paper presents a
preliminary trajectory design for the NuSol mission in order to accomplish the sci-
ence goals, taking into account specified mission cost constraints, a given launch
window, and an overall mission duration. Numerical simulations are presented to
compare different mission scenarios and to identify a trajectory design that realizes
the science goals of the mission. 

2021 MS Thesis

Preliminary mission design for proposed NuSol probe 

Author: K. Messick 

Abstract: A solar neutrino detector has never flown in space. NuSol is a proposed mission to fly a solar neutrino detector close to the Sun in order to conduct unique science experiments that cannot be realized by detectors on Earth. This research presents a preliminary trajectory design for the NuSol mission in order to accomplish the science goals, taking into account operational and specified mission cost constraints, given launch window, and an overall mission duration. To quickly check through a diverse design space of possible mission solutions, a mission design algorithm was developed in MATLAB. The mission design procedure used in this thesis is based on the standard patched-conics methodology to break the mission into a sequence of two-body problems, starting with a hyperbolic Earth escape trajectory and followed by elliptic heliocentric orbits yielding multiple planetary arrival phases. Minimization of the final perihelion is done by utilizing multiple consecutive gravity assist (GA) maneuvers to reshape the initial trajectory after a launch and departure from Earth. As launch costs prove to be a substantial share of the overall mission cost, the study is restricted to initial launch energies which equal 100 km2/s or less. This study provides insight on the closest reachable distance to the Sun when given a specified wet mass and launch vehicle. The work also addresses many issues in trade offs that arise in multi-GA maneuver mission design studies. These issues include mass trade
offs at launch as well as during the heliocentric transfer when comparing ballistic and powered GA maneuvers. One of the greatest challenges the research works to overcome is the computational time and resources that are required when analyzing a vast mission design space. The results for the study indicate that a currently available launch vehicle can deploy the 1,400 kg spacecraft housing the neutrino detector in a Earth-Venus transfer orbit, which will eventually reach below 20 Solar Radii within the stipulated time of 5 years.