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Volumn 4, Issue , 2007, Pages 3530-3539
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Test facility development for the 15,000 lb thrust Peregrine hybrid sounding rocket
a,e,f a,b,f a,b,f a,e,f a,e,f a,e,f b,c,f c,d,f d,f
e
AIAA
(United States)
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Author keywords
[No Author keywords available]
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Indexed keywords
LIQUID FUELS;
NASA;
OXIDANTS;
TEST FACILITIES;
THRUST REVERSAL;
FLIGHT VEHICLES;
HYBRID SOUNDING ROCKETS;
LIQUIFYING FUEL;
MULTIPLE OXIDIZERS;
SOUNDING ROCKETS;
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EID: 36749076021
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.2007-5358 Document Type: Conference Paper |
Times cited : (11)
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References (6)
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