2 edition of **Numerical modeling of on-orbit propellant motion resulting from an impulsive acceleration** found in the catalog.

Numerical modeling of on-orbit propellant motion resulting from an impulsive acceleration

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- 23 Currently reading

Published
**1987** by National Aeronautics and Space Administration, For sale by the National Technical Information Service in [Washington, DC], [Springfield, Va .

Written in English

- Fluid dynamics.

**Edition Notes**

Other titles | Numerical modeling of on orbit propellant motion resulting from an impulsive acceleration. |

Statement | John C. Aydelott ... [et al.]. |

Series | NASA technical memorandum -- 89873. |

Contributions | Aydelott, John C., United States. National Aeronautics and Space Administration. |

The Physical Object | |
---|---|

Format | Microform |

Pagination | 1 v. |

ID Numbers | |

Open Library | OL18033374M |

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Get this from a library. Numerical modeling of on-orbit propellant motion resulting from an impulsive acceleration. [John C Aydelott; United States. National Aeronautics and Space Administration.;]. Numerical modeling of on-orbit propellant motion resulting from an impulsive acceleration. JOHN AYDELOTT, RAYMOND MJOLSNESS, A multidomain and multidimensional numerical analysis of flow in fuelside preburner, high pressure turbine, hot gas manifold and main injector assembly of the Space Shuttle main engine Modeling shock/boundary.

Although the shuttle/Centaur development activity has been suspended, the numerical modeling techniques are available to predict on-orbit liquid motion resulting from impulsive accelerations for.

Phase field modeling of liquid jets in low gravity Numerical modeling of on-orbit propellant motion resulting from an impulsive acceleration to predict on-orbit liquid motion resulting Author: David Chato. Section 3 presents a single impulsive control law to correct relative angular momentum and energy for formation design.

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