Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
doi 10.2322/tastj.14.pb_13
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Integrated Flight/Propulsion Control System Design Based on a Decentralized, Hierarchical Approach

1989English

Installed Performance Assessment of a Boundary Layer Ingesting Distributed Propulsion System at Design Point

2016English

A Redundancy and Operation of Power Control System for a Deep-Space Small Probe

Journal of Automation and Control Engineering
2016English

Estimation of Flight Path Deviations for SAR Radar Installed on UAV

Metrology and Measurement Systems
2016English

Remote Infrared Imaging of the Space Shuttle During Hypersonic Flight: HYTHIRM Mission Operations and Coordination

2011English

A Dual Mode Propulsion System for Small Satellite Applications

Aerospace
Aerospace Engineering
2018English

Computational Modeling of the Trailmaster Procyon System

English

Flight Control System Using Backstepping Method for Space Transportation System

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
2012English

Development Study on LH2/LOX Rocket Propulsion System in the Institute of Space and Astronautical Science.

Journal of the Japan Society for Aeronautical and Space Sciences
1985English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy