[KNYGA][B] Spacecraft propulsion

CD Brown - 1996 - books.google.com
This book is a product of my spacecraft design course at Colorado University. Its primary
purpose is to teach. To that end, the subjects are explained as clearly as possible with …

A review of contemporary solid rocket motor performance prediction techniques

WH Miller, DK Barrington - Journal of Spacecraft and Rockets, 1970 - arc.aiaa.org
THIS paper reviews state-of-the-art techniques for pre-dicting performance of contemporary
solid rocket motor designs. Analytical techniques used in these predictions mathematically …

[KNYGA][B] Solid rocket motor performance analysis and prediction

WH Miller - 1971 - books.google.com
The initial phase of a solid rocket motor development program is typified by numerous
parametric studies conducted to optimize the design. Fabrication problems, specified motor …

A unified model for the acceleration-produced burning rate augmentation of metalized solid propellants

CT Crowe - Combustion science and Technology, 1972 - Taylor & Francis
Experiments have shown that acceleration of metalized composite propellants can affect an
increased burning rate. The pressure-time trace of an accelerated propellant, which under …

A photographic and analytic study of composite propellant combustionin an acceleration field

PG Willoughby, CT Crowe, KL Baker - Journal of Spacecraft and …, 1971 - arc.aiaa.org
IT has long been known that spinning an internal-burning solid-propellant rocket motor
about its longitudinal axis for directional stability can significantly affect the motor's internal …

An investigation of the swirling flow in a spinning end-burning rocket

R DUNLAP - AIAA Journal, 1969 - arc.aiaa.org
NUMEROUS tests have shown that spinning a solid propellant rocket about its longitudinal
axis to promote fligfit stability may alter considerably its internal ballistics. The spinning …

Effects of the acceleration vector on transient burning rate of an aluminized solid propellant.

GB NORTHAM - Journal of Spacecraft and Rockets, 1971 - arc.aiaa.org
MANY solid-propellant rocket vehicles have been de-veloped that use spin or inertial
stabilization to provide dynamic stability and reduce dispersion due to thrust misalinement in …

Mechanism of Influence of High‐Speed Self‐Spin on Ignition Transients for a Solid Rocket Motor: a Numerical Simulation

D Guan, S Li, X Sui, N Wang - Propellants, Explosives …, 2020 - Wiley Online Library
High‐speed self‐spin is one of extreme working conditions that alters ignition internal
ballistic performance and can induce ignition abnormalities. To demonstrate the studies on …

The effect of acceleration on composite propellant combustion

D Cowles, D Netzer - Combustion Science and Technology, 1971 - Taylor & Francis
The effects or burn time (web thickness) and acceleration on the weight, form and chemical
composition of the molten metallic material on or adjacent to the burning surface of …

Burning rate acceleration sensitivity of double-base propellant

MJ Bulman, DW Netzer - AIAA Journal, 1970 - arc.aiaa.org
ANUMBER of investigators1" 7 have considered the effects of acceleration on the burning
rates of solid propellants. Analytical investigations1'3'8-9 and most experimental …