Grumman SSM-N-6 Rigel

[Deleted member 2278]

Grumman SSM-N-6 Rigel

Some Rigel related items that may be of interest:

NASA Technical Reports Server (NTRS) 19930086621: Wind-tunnel Investigation at Mach Numbers of 1.5 and 2.0 of a Canard Missile Configuration : NASA Technical Reports Server (NTRS) : Free Download, Borrow, and Streaming : Internet Archive

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The world's most significant and magnificent aircraft : evolution of the modern airplane : Thurston, David B : Free Download, Borrow, and Streaming : Internet Archive

xix, 262 p. : 26 cm

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Aviation Week 1955-04-25 : Aviation Week : Free Download, Borrow, and Streaming : Internet Archive

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DTIC AD0036129: RAMJET TECHNOLOGY. CHAPTER 10. DESIGN OF BAFFLE-TYPE COMBUSTORS : Defense Technical Information Center : Free Download, Borrow, and Streaming : Internet Archive

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DTIC AD0041743: RAMJET TECHNOLOGY. CHAPTER 7. AIR-FUEL MIXTURE PREPARATION : Defense Technical Information Center : Free Download, Borrow, and Streaming : Internet Archive

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NASA Technical Reports Server (NTRS) 19930086772: Effect of design changes and operating conditions on combustion and operational performance of a 28-inch diameter Ram-jet engine / T. B. Shillito and Shigeo Nakanishi : NASA Technical Reports Server (

The results of an altitude test-chamber investigation of the effects of a number of design changes and operating conditions on altitude peformance of a 28-inch...

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NASA Technical Reports Server (NTRS) 19930086213: Altitude-test-chamber Investigation of Performance of a 28-inch Ram-jet Engine I : Combustion and Operational Performance of Four Combustion-chamber Configurations : NASA Technical Reports Server (NTR

An altitude-test-chamber investigation of a 28-inch-diameter ram-jet engine at a simulated flight Mach number of approximately 2.0 for altitudes of 40,000 to...

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NASA Technical Reports Server (NTRS) 19930086341: Altitude Test Chamber Investigation of Performance of a 28-inch Ram-jet Engine II : Effects of Gutter Width and Blocked Area on Operating Range and Combustion Efficiency : NASA Technical Reports Serve

Altitude-test-chamber investigation of effects of flame-holder blocked area and gutter width on performance of 28-inch diameter ram jet at simulated flight...

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NASA Technical Reports Server (NTRS) 19930086636: Altitude-test-chamber investigation of performance of a 28-inch ram-jet engine III : combustion and operational performance of three flame holders with a center pilot burner : NASA Technical Reports S

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NASA Technical Reports Server (NTRS) 19930086611: Altitude-test-chamber Investigation of Performance of a 28-inch Ram-jet Engine IV : Effect of Inlet-air Temperature, Combustion-chamber-inlet Mach Number, and Fuel Volatility on Combustion Performance

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[NMaude]

Excellent!