Guidance and Navigation Challenges for a Mars Ascent Vehicle [PDF]
This work presents studies and analysis in support of a Mars Ascent Vehicle as part of a Martian Sample Return campaign. The vehicle design has been ongoing, with rapid development of a 6 Degree of Freedom simulation to capture full vehicle dispersions ...
Anzalone, Evan +3 more
core +1 more source
An investigation of networking techniques for the ASRM facility [PDF]
This report is based on the early design concepts for a communications network for the Advanced Solid Rocket Motor (ASRM) facility being built at Yellow Creek near Iuka, MS.
Moorhead, Robert J., II +2 more
core +1 more source
Radiation/convection coupling in rocket motor and plume analysis [PDF]
A method for describing radiation/convection coupling to a flow field analysis was developed for rocket motors and plumes. The three commonly used propellant systems (H2/O2, RP-1/O2, and solid propellants) radiate primarily as: molecular emitters, non ...
Farmer, R. C., Saladino, A. J.
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The investigation of flame spreading over the surface of igniting solid propellants Final summary report [PDF]
Flame spreading over surface of igniting solid propellants in different gas mixtures at various ...
Magee, R. S., Mc Alevy, R. F., III
core +1 more source
Immersive Virtual Reality for Stroke Rehabilitation: Linking Clinical and Digital Measures of Motor Recovery-A Pilot Study. [PDF]
Bioengineering (Basel)Ion LA +9 more
europepmc +1 more source
A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Sci RepLi T, He H, Yu N, Sun X, Cai G.
europepmc +1 more source
Lightweight structural design of a bolted case joint for the space shuttle solid rocket motor [PDF]
The structural design of a bolted joint with a static face seal which can be used to join Space Shuttle Solid Rocket Motor (SRM) case segments is given.
Bush, Harold G. +2 more
core +1 more source
Development of a combustion visualisation hybrid rocket motor
, 2017 The Phoenix Hybrid Sounding Rocket Programme in the University of KwaZulu-Natal's Mechanical Engineering department has so far only utilised pure paraffin wax and nitrous oxide as the propellant combination in their hybrid rockets. Knowledge of regression rate behaviour is required for the design and performance characterisation of hybrid rocket ...
Theba, R, Veale, KL, Bemont, CP
openaire +1 more source
Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]
Polymers (Basel)Meiirbekov M +7 more
europepmc +1 more source
The aerodynamic challenges of SRB recovery [PDF]
Recovery and reuse of the Space Shuttle solid rocket boosters was baselined to support the primary goal to develop a low cost space transportation system.
Bacchus, D. L. +2 more
core +1 more source