Designer's Guide and Computer Program for Ablative Materials in Liquid Rocket Thrust Chambers

doi 10.21236/ad0816546
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

Cooling of High-Pressure Rocket Thrust Chambers With Liquid Oxygen

Journal of Spacecraft and Rockets
SpacePlanetary ScienceAerospace Engineering
1981English

Coolant Pressure Losses in Regenerative Cooled Liquid Rocket Chambers and Nozzles

Houille Blanche
Water ScienceTechnology
1963English

Hardware Designer's Guide to Fault Attacks

IEEE Transactions on Very Large Scale Integration (VLSI) Systems
HardwareElectronic EngineeringElectricalArchitectureSoftware
2013English

Thrust Magnitude Control of Solid Rocket Motors

Journal of the Japan Society for Aeronautical and Space Sciences
1970English

A Fashion Designer's Feeling of Textile Materials

Sen'i Gakkaishi
Materials ScienceIndustrialPolymersManufacturing EngineeringPlasticsChemical Engineering
1983English

Experimental Demonstration of Magnetic Thrust Chamber for a Laser Fusion Rocket

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

Numerical Simulation of a Pintle Variable Thrust Rocket Engine

DEStech Transactions on Computer Science and Engineering
2019English

Raptor Management Information System : Users' Guide for an Interactive REX2 Computer Program /

1982English

Guide for Licensing Evaluations Using CRAC2: A Computer Program for Calculating Reactor Accident Consequences

1988English

Amanote Research

Note-taking for researchers

Follow Amanote

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

Privacy PolicyRefund Policy