H-II rocket.

Rocket Apparatus

Ultracompact H Ii Regions

RESUMEN Discutimos algunos resultados observacionales recientes sobre regiones H II ultracompactas. En particular, discutimos la emisión extendida de algunas regiones H II UC y el descubrimiento de una nueva clase, denominada regiones H II " hipercompactas ". Además, describimos la obtención de la estructura de densidad usando la técnica del análisis deí ındice espectral. ABSTRACT We discuss so...

Hybrid Rocket Propulsion Technology for Sounding Rocket Development

Hybrid combustion technology has recently been employed in the sounding rocket developments to support the science experiments of academic applications and the establishment of a viable flight test platform for space components development. Due to its safety nature in material handling and combustion processes, hybrid rockets are suitable for university and research institute environments for a...

Rocket Propulsion Establishment

MicroLaunch: The Electric Rocket

MicroLaunch is a potentially game changing development for access to space for nano and pico satellites (1 to 50kg) which today are being used in ever greater numbers by commercial providers (e.g. Skybox Imaging, Planet Labs), universities, domestic space agencies and military research organisations. These satellites are poorly served by today’s launch marcet, generally having to ‘piggy back’ a...