enow.com Web Search

Search results

  1. Results from the WOW.Com Content Network
  2. Delta-v budget - Wikipedia

    en.wikipedia.org/wiki/Delta-v_budget

    Their one-way delta-v budgets from LEO range upwards from 3.8 km/s (12,000 ft/s), which is less than 2/3 of the delta-v needed to reach the Moon's surface. [10] But NEOs with low delta-v budgets have long synodic periods , and the intervals between times of closest approach to the Earth (and thus most efficient missions) can be decades long.

  3. File:Solar system delta v map.svg - Wikipedia

    en.wikipedia.org/wiki/File:Solar_system_delta_v...

    Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.

  4. Delta-v - Wikipedia

    en.wikipedia.org/wiki/Delta-v

    Thus it can be shown that, provided the exhaust velocity is fixed, this means that delta-v can be summed: When m 1, m 2 are the mass ratios of the maneuvers, and v 1, v 2 are the delta-v of the first and second maneuvers = / / = + = / = where V = v 1 + v 2 and M = m 1 m 2. This is just the rocket equation applied to the sum of the two maneuvers.

  5. Low-energy transfer - Wikipedia

    en.wikipedia.org/wiki/Low-energy_transfer

    Belbruno's routes from low Earth orbit require a 3.1 km/s burn for trans lunar injection, a delta-v saving of not more than 0.4 km/s. However, the latter require no large delta- v change after leaving low Earth orbit, which may have operational benefits if using an upper stage with limited restart or in-orbit endurance capability, which would ...

  6. Free-return trajectory - Wikipedia

    en.wikipedia.org/wiki/Free-return_trajectory

    It takes 250 days (0.68 years) in the transit to Mars, and in the case of a free-return style abort without the use of propulsion at Mars, 1.5 years to get back to Earth, at a total delta-v requirement of 3.34 km/s. Zubrin advocates a slightly faster transfer, that takes only 180 days to Mars, but 2 years back to Earth in case of an abort.

  7. Two-stage-to-orbit - Wikipedia

    en.wikipedia.org/wiki/Two-stage-to-orbit

    [1] An advantage over three or more stages is a reduction in complexity and fewer separation events, which reduces cost and risk of failure. [2] Importance of Structural coefficient and I SP for Single-Stage-to-Orbit (SSTO) and restricted stage Two-Stage-to-Orbit (TSTO) vehicles. Based on a LEO mission of Delta v = 9.1 km/s and payload mass ...

  8. Kerbal Space Program - Wikipedia

    en.wikipedia.org/wiki/Kerbal_Space_Program

    Kerbal Space Program (KSP) is a space flight simulation video game developed by Mexican studio Squad for Linux, macOS, Windows, PlayStation 4, PlayStation 5, Xbox Series X/S and Xbox One. In the game, players direct the space program of a species of green humanoid aliens known as "Kerbals".

  9. Gravity loss - Wikipedia

    en.wikipedia.org/wiki/Gravity_loss

    The actual acceleration of the craft is a-g and it is using delta-v at a rate of a per unit time. Over a time t the change in speed of the spacecraft is (a-g)t, whereas the delta-v expended is at. The gravity loss is the difference between these figures, which is gt. As a proportion of delta-v, the gravity loss is g/a.