Jove
Visualize
Contact Us
JoVE
x logofacebook logolinkedin logoyoutube logo
ABOUT JoVE
OverviewLeadershipBlogJoVE Help Center
AUTHORS
Publishing ProcessEditorial BoardScope & PoliciesPeer ReviewFAQSubmit
LIBRARIANS
TestimonialsSubscriptionsAccessResourcesLibrary Advisory BoardFAQ
RESEARCH
JoVE JournalMethods CollectionsJoVE Encyclopedia of ExperimentsArchive
EDUCATION
JoVE CoreJoVE BusinessJoVE Science EducationJoVE Lab ManualFaculty Resource CenterFaculty Site
Terms & Conditions of Use
Privacy Policy
Policies

Related Experiment Videos

How we will go to Mars.

B N Kiforenko1, I Yu Vasil'ev

  • 1Taras Shevchenko Kyiv University, Kyiv, Ukraine. kifor@univ.kiev.ua

Acta Astronautica
|October 14, 2003
PubMed
Summary
This summary is machine-generated.

Ejecting waste from a spacecraft

Related Concept Videos

You might also read

Related Articles

Articles linked to this work by shared authors, journal, and citation graph.

Sort by
Same journal

Rendering knowledge graphs from aerospace dentistry processes for clinical decision support systems.

Acta astronautica·2025
Same journal

Interstellar space biology via Project Starlight.

Acta astronautica·2023
Same journal

How businesses are working together to deliver NASA/JPL-designed ventilators to the world in the fight against COVID-19.

Acta astronautica·2022
Same journal

A Geospatial Artificial Intelligence and satellite-based earth observation cognitive system in response to COVID-19.

Acta astronautica·2022
Same journal

Isolation and confinement due to the COVID-19 pandemic: Lessons for human spaceflight.

Acta astronautica·2022
Same journal

Data-driven CFD Scaling of Bioinspired Mars Flight Vehicles for Hover.

Acta astronautica·2022
See all related articles

Area of Science:

  • Spacecraft engineering
  • Astrodynamics
  • Life support systems

Background:

  • Manned interplanetary missions require significant initial mass, posing challenges for launch and trajectory.
  • Current life support systems (LSS) generate waste that contributes to this mass.
  • Reducing initial spacecraft mass is crucial for enabling long-duration missions, such as to Mars.

Purpose of the Study:

  • To investigate the efficiency of ejecting waste generated by a spacecraft's life support system (LSS).
  • To determine if waste ejection can reduce the initial mass required for a manned interplanetary mission.
  • To assess the feasibility of waste ejection for enabling early manned Mars missions.

Main Methods:

  • Simulation of an optimal control problem for spacecraft maneuver using an impulsive approximation for interplanetary trajectories.

Related Experiment Videos

  • Decomposition of the optimal control problem into hierarchical 'outer' and 'inner' subproblems.
  • Analysis of the problem structure using Pontryagin's Maximum principle.
  • Main Results:

    • Numerical results demonstrate the efficiency of waste ejection for reducing spacecraft initial mass.
    • The study confirms that waste ejection significantly decreases the required initial mass for Earth-Mars transfer trajectories.
    • The findings support the theoretical possibility of early manned Mars missions through waste ejection.

    Conclusions:

    • Waste ejection from the LSS is a viable strategy for reducing spacecraft initial mass.
    • This approach can make early manned Mars missions feasible without necessitating advanced biological LSS.
    • The study provides a theoretical basis for implementing waste ejection systems in future interplanetary spacecraft.