Mr. Kyle,I think I have found a reference to the "Titan V" as "Growth Titan IV" in a report entitled "Space Station Heavy Lift Launch Vehicle Utilization" on NTRS ( http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880011804.pdf ). The diagram (showing a LDC Titan with two RSRMs) is on the 18th page of the PDF and gives a height of 265.5 feet, and a LEO payload of 95k lbs.
Arcturus and Aldeberan images.
Quote from: Jim Davis on 06/11/2016 09:29 pmArcturus and Aldeberan images.On page 17 of the 28 March 1960 issue of Missiles and Rockets (plutogno provides a link) you'll find an article about the report by Dandridge Cole when Aldeberan was proposed.Be warned, though, that you can disappear into the M&R archive for hours; it's as bad as NTRS the first time you encounter it!
It started as a monthly but from July 1958 was a weekly. Go to page 707 of the PDF.
I have question on The Titan V studies had Martin Marietta study in 1988 a Titan with cryogenic core stage or not and this is mix up with cryogenic Titan study from James A. Martin ? on several web pages label Titan V as "Ariane 5 like booster" with 2 UA1207 and cryogenic core stagei could trace that down to Astonautix http://www.astronautix.com/t/titan5.htmlMartin Study 1988 as alternative to NLS.Thrust: 16,533.60 kN (3,716,901 lbf). Gross mass: 1,138,660 kg (2,510,310 lb). Height: 72.00 m (236.00 ft). Diameter: 6.00 m (19.60 ft).it use one engine "PW 1000000 lb LH2" for core stage trust 4,457.100 kN (vac), Isp: 425 sec. sadly there no reverence were this data came fromAlso i found in German aerospace magazine from 1991a article about 1990s US spaceflight development, with this phrase "also is manufacture study a Titan 5 with cryogenic core" Again no reverence what so ever on this.
Von Braun's team actually began contract discussions for "Saturn Titan" with Martin during mid 1959.
Quote from: edkyle99 on 06/12/2016 02:40 pmVon Braun's team actually began contract discussions for "Saturn Titan" with Martin during mid 1959.Saturn A-1 was proposed with Titan as a second stage: http://www.astronautix.com/s/saturna-1.htmlThe first Saturns were even built with a 10' diameter interstage structure.
found Martin Marietta corp. studythey mention a Titan IIIF/stretched TranstageGot someone more info on that Transtage?Source:Study of Direct Versus Orbital entry for mars missionvolume III Launch Vehicle Performance and Flight MechanicsNASA CR-66661196800223161.pdf