V-400 Dal/SA-5 Griffon - Revision history

The Wrigley Guerrilla at 13:43, 22 October 2019

2019-10-22T13:43:59Z

← Older revision		Revision as of 13:43, 22 October 2019
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	Status: Cancelled 1973.		Status: Cancelled 1973.

-	Payload: 250 kg (550 lb).	+	Payload: 250 kg (550 lbs).

-	Gross mass: 8,757 kg (19,305 lb).	+	Gross mass: 8,757 kg (19,305 lbs).

-	~~Height~~: 14.20 m (46.50 ft).	+	Length: 14.20 m (46.50 ft).

	Diameter: 0.65 m (2.13 ft).		Diameter: 0.65 m (2.13 ft).

The Wrigley Guerrilla at 16:24, 21 October 2019

2019-10-21T16:24:29Z

← Older revision		Revision as of 16:24, 21 October 2019
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	== See also ==		== See also ==
-
-	~~[[S-25 Berkut/SA-1 Guild]]~~
-
-	~~[[S-75 Dvina/SA-2 Guideline]]~~
-
-	~~[[S-125 Neva/SA-3 Goa]]~~
-
-	~~[[2K11 Krug/SA-4 Ganef]]~~
-
-	~~[[S-200 Angara/SA-5 Gammon]]~~
-
-	~~[[2K12 Kub/SA-6 Gainful]]~~

	[[V-1000/Griffon]]		[[V-1000/Griffon]]

The Wrigley Guerrilla at 22:47, 4 April 2019

2019-04-04T22:47:50Z

← Older revision		Revision as of 22:47, 4 April 2019
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	[[S-75 Dvina/SA-2 Guideline]]		[[S-75 Dvina/SA-2 Guideline]]
		+
		+	[[S-125 Neva/SA-3 Goa]]

	[[2K11 Krug/SA-4 Ganef]]		[[2K11 Krug/SA-4 Ganef]]

The Wrigley Guerrilla at 22:37, 4 April 2019

2019-04-04T22:37:05Z

← Older revision		Revision as of 22:37, 4 April 2019
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	[[S-75 Dvina/SA-2 Guideline]]		[[S-75 Dvina/SA-2 Guideline]]

-	[[2K11 Krug/SA-3 Ganef]]	+	[[2K11 Krug/SA-4 Ganef]]

	[[S-200 Angara/SA-5 Gammon]]		[[S-200 Angara/SA-5 Gammon]]

The Wrigley Guerrilla at 21:17, 3 April 2019

2019-04-03T21:17:31Z

← Older revision		Revision as of 21:17, 3 April 2019
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	[[2K12 Kub/SA-6 Gainful]]		[[2K12 Kub/SA-6 Gainful]]
		+
		+	[[V-1000/Griffon]]

	[[A-35 Aldan]]		[[A-35 Aldan]]

The Wrigley Guerrilla at 20:38, 3 April 2019

2019-04-03T20:38:19Z

← Older revision		Revision as of 20:38, 3 April 2019
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	8. Ramjet engine M M Bondaryuk.		8. Ramjet engine M M Bondaryuk.
		+

	OKB-301 Deputy Director M M Pashimin led the team developing the V-400 surface-to-air missile. The V-400 was to be a two-stage rocket with the index 5V11. The rocket itself was to be theoretically capable of intercepting targets flying between 1500 and 3000 kph at altitudes from 5 to 30 km. Development had begun at the beginning of 1955, even before the decree was issued. The Soviet Ministers established the final TTT specification for the system on 17 August 1956 in decree 1148-581. However due to the high level of technical innovation, the draft project was not completed until April 1957. Two variants were proposed, consisting of either two liquid propellant rocket stages, or a rocket booster with a ramjet second stage. Isayev designed the three-chamber booster engine for either design. During trials an alternate solid booster was also tested, which had a shorter burn time and no control of thrust during the boost. This was the PRD-70 designed by I I Kartukov at KB-2 Factory 81.		OKB-301 Deputy Director M M Pashimin led the team developing the V-400 surface-to-air missile. The V-400 was to be a two-stage rocket with the index 5V11. The rocket itself was to be theoretically capable of intercepting targets flying between 1500 and 3000 kph at altitudes from 5 to 30 km. Development had begun at the beginning of 1955, even before the decree was issued. The Soviet Ministers established the final TTT specification for the system on 17 August 1956 in decree 1148-581. However due to the high level of technical innovation, the draft project was not completed until April 1957. Two variants were proposed, consisting of either two liquid propellant rocket stages, or a rocket booster with a ramjet second stage. Isayev designed the three-chamber booster engine for either design. During trials an alternate solid booster was also tested, which had a shorter burn time and no control of thrust during the boost. This was the PRD-70 designed by I I Kartukov at KB-2 Factory 81.

The Wrigley Guerrilla at 20:38, 3 April 2019

2019-04-03T20:38:02Z

← Older revision		Revision as of 20:38, 3 April 2019
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	The development plan called for completion of breadboard systems by the second quarter of 1956, the first test articles by the first quarter of 1958, and factory trials completed by the second quarter of 1959. Lavochkin's OKB-301 was the prime contractor, with principle subcontractors being:		The development plan called for completion of breadboard systems by the second quarter of 1956, the first test articles by the first quarter of 1958, and factory trials completed by the second quarter of 1959. Lavochkin's OKB-301 was the prime contractor, with principle subcontractors being:

-	Active radar homing system, A B Sledushkin at NII-17 MRTP	+	1. Active radar homing system, A B Sledushkin at NII-17 MRTP,

-	On-board radar, V V Samara	+	2. On-board radar, V V Samara,

-	Data link, N I Belov	+	3. Data link, N I Belov,

-	On-board computer, Bazilevskiy at NIEI MRTP	+	4. On-board computer, Bazilevskiy at NIEI MRTP,

-	Liquid propellant engine, Isayev in collaboration with Kosberg	+	5. Liquid propellant engine, Isayev in collaboration with Kosberg,

-	Warhead, V A Sukhikh at KB NII-6 MSKhM	+	6. Warhead, V A Sukhikh at KB NII-6 MSKhM,

-	Launcher V P Barmin	+	7. Launcher V P Barmin,

-	Ramjet engine M M Bondaryuk.	+	8. Ramjet engine M M Bondaryuk.

	OKB-301 Deputy Director M M Pashimin led the team developing the V-400 surface-to-air missile. The V-400 was to be a two-stage rocket with the index 5V11. The rocket itself was to be theoretically capable of intercepting targets flying between 1500 and 3000 kph at altitudes from 5 to 30 km. Development had begun at the beginning of 1955, even before the decree was issued. The Soviet Ministers established the final TTT specification for the system on 17 August 1956 in decree 1148-581. However due to the high level of technical innovation, the draft project was not completed until April 1957. Two variants were proposed, consisting of either two liquid propellant rocket stages, or a rocket booster with a ramjet second stage. Isayev designed the three-chamber booster engine for either design. During trials an alternate solid booster was also tested, which had a shorter burn time and no control of thrust during the boost. This was the PRD-70 designed by I I Kartukov at KB-2 Factory 81.		OKB-301 Deputy Director M M Pashimin led the team developing the V-400 surface-to-air missile. The V-400 was to be a two-stage rocket with the index 5V11. The rocket itself was to be theoretically capable of intercepting targets flying between 1500 and 3000 kph at altitudes from 5 to 30 km. Development had begun at the beginning of 1955, even before the decree was issued. The Soviet Ministers established the final TTT specification for the system on 17 August 1956 in decree 1148-581. However due to the high level of technical innovation, the draft project was not completed until April 1957. Two variants were proposed, consisting of either two liquid propellant rocket stages, or a rocket booster with a ramjet second stage. Isayev designed the three-chamber booster engine for either design. During trials an alternate solid booster was also tested, which had a shorter burn time and no control of thrust during the boost. This was the PRD-70 designed by I I Kartukov at KB-2 Factory 81.

The Wrigley Guerrilla: /* See also */

2019-04-03T17:36:29Z

The Wrigley Guerrilla: /* See also */

2019-04-03T17:36:15Z

The Wrigley Guerrilla at 11:51, 3 April 2019

2019-04-03T11:51:49Z

← Older revision		Revision as of 11:51, 3 April 2019
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	[[S-200 Angara/SA-5 Gammon]]		[[S-200 Angara/SA-5 Gammon]]
-
-	~~[[S-300 Weapons System family/SA-10 Grumble]]~~
-
-	~~[[S-400 Triumf/SA-21 Growler]]~~

	[[A-35 Aldan]]		[[A-35 Aldan]]

← Older revision		Revision as of 17:36, 3 April 2019
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	[[S-75 Dvina/SA-2 Guideline]]		[[S-75 Dvina/SA-2 Guideline]]
		+
		+	[[2K11 Krug/SA-3 Ganef]]

	[[S-200 Angara/SA-5 Gammon]]		[[S-200 Angara/SA-5 Gammon]]
		+
		+	[[2K12 Kub/SA-6]]

	[[A-35 Aldan]]		[[A-35 Aldan]]
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	[[Soviet/Russian Strategic Communication/Warfare Units]]		[[Soviet/Russian Strategic Communication/Warfare Units]]
-

	== Sources ==		== Sources ==

	Encyclopedia Astronautica, Wikipedia		Encyclopedia Astronautica, Wikipedia

← Older revision		Revision as of 17:36, 3 April 2019
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	[[S-200 Angara/SA-5 Gammon]]		[[S-200 Angara/SA-5 Gammon]]

-	[[2K12 Kub/SA-6]]	+	[[2K12 Kub/SA-6 Gainful]]

	[[A-35 Aldan]]		[[A-35 Aldan]]