Analysis of Low $\Delta V$ Spacecraft Missions to Oort Cloud Comet C/2014 UN$_{271}
Comet C/2014 UN$_{271}$, alternative designation 'BB' after its discoverers 'Bernardinelli/Bernstein', and commonly referred to as UN$_{271}$, is an extreme case on two fronts, firstly its solar distance on discovery ($>$ 29 au) and secondly the size of its nucleus (137$\pm$ 1...
Saved in:
Main Authors: | , |
---|---|
Format: | Journal Article |
Language: | English |
Published: |
11-10-2022
|
Subjects: | |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Summary: | Comet C/2014 UN$_{271}$, alternative designation 'BB' after its discoverers
'Bernardinelli/Bernstein', and commonly referred to as UN$_{271}$, is an
extreme case on two fronts, firstly its solar distance on discovery ($>$ 29 au)
and secondly the size of its nucleus (137$\pm$ 15 km). With an aphelion
distance of $\sim$33,000 au (w.r.t. the solar system barycentre) and an orbital
period $\sim$2 million years, it is definitely an object from the solar
system's Oort cloud, and also by a good measure the largest Oort cloud object
ever observed. In situ observation of UN$_{271}$ would be of considerable
scientific importance. Unlike most Oort cloud comets which have been discovered
for the first time only as they near the inner solar system, UN$_{271}$ was
discovered early enough to provide adequate advanced warning to plan for such a
mission. In this paper we describe the various methods for reaching UN$_{271}$
during the period around its perihelion and ecliptic plane passage, with both
flyby and rendezvous options; exploiting direct transfers, Jupiter powered
gravitational assists (GA) or alternatively a series of GAs of the inner
planets. Viable flyby and rendezvous trajectories are found, especially using
the NASA Space Launch System (SLS) as the launch vehicle. |
---|---|
DOI: | 10.48550/arxiv.2210.05190 |