Aerospike Nozzle - Solid Rocket Motor Static Firing

Discussions of motors from single-use and RMS solid propellants to hybrid propellants

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CATO
Mr Smiley
Mr Smiley
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Aerospike Nozzle - Solid Rocket Motor Static Firing

Postby CATO » Wed Aug 12, 2015 9:02 pm

eAc (Environmental Aeroscience Corp) developed and fired the first solid propellant Aerospike motor in 2003. Aerospike nozzles are designed to be altitude compensating and self adjust the expansion ratio making them extremely useful for ground-launched sounding rockets. This feature is specifically useful for long burn hybrid rocket applications. Several design verification tests firings using short burn solid propellants, with the goal of applying the technology to the long burn Hybrid motors.

"In thrust we trust"

AMRS 21 L3
TRA 07459 L3

Impulse:
2018: 14,767 Ns (44% N)
Ns 17: 5,973; 16: 34,558; 15: 35,955; 14: 6,016; 13: 10,208
PB - Gorilla N2717WC, H: 10,260', S: 1.14M

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