List of V-2 test launches

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http://en.wikipedia.org/wiki/List_of_V-2_test_launches

World War II test launches of the A4 rocket, better known as the V-2 rocket, were made at Test Stand VII, Blizna and Tuchola Forest using experimental and production rockets fabricated at Peenemünde and at the Mittelwerk. Post war test launches were conducted at Cuxhaven, White Sands Proving Grounds, Cape Canaveral, and Kapustin Yar.

List of test launches at Peenemünde and the Greifswalder Oie

Launches of A4b

Launch Sites:

P-VI = Test Stand VI (Prüfstand VI)
P-VII = Test Stand VII (Prüfstand VII)
P-X = Test Stand X (Prüfstand X)
P-XII = Test Stand XII (Prüfstand XII)
Oie = Greifswalder Oie, a small island used for vertical launches
Karlshagen = area of destroyed settlement Karlshagen after air raid on 17 August 1943
Rail = Launches from a train

Blizna test launch list

Tuchola forest test launch list

Launches at Operation Backfire near Cuxhaven

Date	Time	Maximum height	Length of flight	Remarks
2 October 1945	14h41	69.4 km	249.4 km
4 October 1945	14h16	17.4 km	24 km	Engine failure shortly after launch
15 October 1945	15h06	64 km	233 km	Some sources indicate launch took place on 14 October 1945

Launches of captured V-2 rockets in the USA after 1945

Rocket number	Time	Launch site	Pad	Maximum altitude (kilometres)	Remarks
1946
1	15 March 1946	White Sands		n/a	Static test firing of V-2 Engine
2	16 April 1946	White Sands	Pad 33	5.5	Radio cut-off 19.5 s after launch, Fin 4 failed prior to cut off
3	10 May 1946	White Sands	Pad 33	112.6	Nominal flight
4	29 May 1946	White Sands	Pad 33	112.1	Nominal flight
5	13 June 1946	White Sands	Pad 33	117.4	Nominal flight
6	28 June 1946	White Sands	Pad 33	107.8	Nose separation failure
7	9 July 1946	White Sands	Pad 33	134.4	Nominal performance
8	19 July 1946	White Sands	Pad 33	4.824	Oxygen pump exploded
9	30 July 1946	White Sands	Pad 33	161.5	Nominal performance
10	15 August 1946	White Sands	Pad 33	6.4	Radio cut-off 16.5 s after launch
11	22 August 1946	White Sands	Pad 33	0	Control failure led to cut-off command at 6.5s
12	10 October 1946	White Sands	Pad 33	173.8	Nominal performance
13	24 October 1946	White Sands	Pad 33	104.6	Sub-normal propulsion performance
14	7 November 1946	White Sands	Pad 33	0.32	Guidance failure preceded emergency cut-off at 31s
15	21 November 1946	White Sands	Pad 33	101.4	Sub-normal propulsion performance
16	5 December 1946	White Sands	Pad 33	152.9	Control system failed at altitude
17	17 December 1946	White Sands	Pad 33	183.4	Rocket exploded at 440s.
1947
18	10 January 1947	White Sands	Pad 33	116.2	Degraded performance led to roll rate of 60 rpm.
19	23 January 1947	White Sands	Pad 33	49.9	Degraded performance led to roll rate of 80 rpm.
20	20 February 1947	White Sands	Pad 33	109.4	Blossom 1 - Propulsion degraded at 55.5s.
21	7 March 1947	White Sands	Pad 33	162.5	Nominal performance
22	1 April 1947	White Sands	Pad 33	129.2	Nominal performance
23	8 April 1947	White Sands	Pad 33	102.2	Nominal performance
24	17 April 1947	White Sands	Pad 33	142.4	Successful test of ram-jet payload
26	15 May 1947	White Sands	Pad 33	135.2	Internal explosion at 64.3s.
H-II # 0	29 May 1947	White Sands	Pad 33	79.3	Hermes II prototype with dummy Organ ramjet test. Lost control after 4s and crashed outside range near Juarez, Mexico.
29	10 July 1947	White Sands	Pad 33	16.25	Early yaw led to termination at 32s.
30	29 July 1947	White Sands	Pad 33	160.7	Near vertical trajectory.
28	6 September 1947	USS Midway		1.5	Operation Sandy. Aircraft carrier launch successful. Exploded at 1524 m
27	9 October 1947	White Sands	Pad 33	156.1	Internal explosion at 83.5s
GE-Sp	20 November 1947	White Sands	Pad 33	26.7	GE technology proving flight
28	8 December 1947	White Sands	Pad 33	104,6	Stable flight but less than planned altitude
1948
34	22 January 1948	White Sands	Pad 33	159.3	Payload separation failure
36	6 February 1948	White Sands	Pad 33	111	Successfully manoeuvred by ground control for first 40s of fligh
39	19 March 1948	White Sands	Pad 33	5.5	Low altitude flight prevented any data recovery
25	2 April 1948	White Sands	Pad 33	144	Three previous launch attempts failed in year prior. Excellent performance
38	19 April 1948	White Sands	Pad 33	56	Faulty steering led to high roll rate and then flight termination
Bumper-1	13 May 1948	White Sands	Pad 33	127.3	Bumper 1 Premature cut-off of WAC 2nd stage
35	27 May 1948	White Sands	Pad 33	139.7	Steady flight with low roll rate
37	11 June 1948	White Sands	Pad 33	62.3	Blossom 2 - Cut-off at 57.7s; payload separation at 96s
40	26 July 1948	White Sands	Pad 33	86.9	Turbine overspeed led to premature propellad cut-off at 61s. 2rpm roll began at 70s
43	5 August 1948	White Sands	Pad 33	165.7	Nominal performance
Bumper-2	19 August 1948	White Sands	Pad 33	13.4	Bumper 2 First stage failed due to propellant flow interruption
33	2 September 1948	White Sands	Pad 33	150.6	Vehicle broke-up at 370s at 84 km altitude.
Bumper-3	30 September 1948	White Sands	Pad 33	150.3	Bumper 3 WAC stage failed
Bumper-4	1 November 1948	White Sands	Pad 33	4.8	Bumper 4 Explosion in tail of V-2
44	18 November 1948	White Sands	Pad 33	145.3	First Hermes B 'Organ' test of ramjet diffuser in place of payload section. Nominal performance.
42	9 December 1948	White Sands	Pad 33	108.4	Vane failure at 22s caused erratic flight
1949
H-II # 1	13 January 1949	White Sands	Pad 33		1st Hermes II test
45	28 January 1949	White Sands	Pad 33	59.9	Defective performance
48	17 February 1949	White Sands	Pad 33	100.6	Nominal performance
Bumper-5	24 February 1949	White Sands	Pad 33	129	Successful flight. Separation of stages at 32.2 km
41	21 March 1949	White Sands	Pad 33	133.5	Blossom 3 - Parachute not ejected
50	11 April 1949	White Sands	Pad 33	87.2	Degraded performance from 43s
Bumper-6	21 April 1949	White Sands	Pad 33	49.9	Premature V-2 cut-off; WAC stage failed to fire
46	5 May 1949	White Sands	Pad 33	8.85	Second Hermes II 'Organ' test of ramjet diffuser in place of payload section
47	14 June 1949	White Sands	Pad 33	133.5	Blossom 4 - Nominal performance.
32	16 September 1949	White Sands	Pad 33	4.2	Blossom 5 - payload. Explosions led to early termination
49	29 September 1949	White Sands	Pad 33	150.8	Nominal performance.
H-II # 2	6 October 1949	White Sands	Pad 33		2nd Hermes II test.
56	18 November 1949	White Sands	Pad 33	123.9	Nominal performance.
31	8 December 1949	White Sands	Pad 33	130.3	Blossom 6 - Excellent performance
1950
53	17 February 1950	White Sands	Pad 33	148.7	Nominal performance.
Bumper-8	24 July 1950	Cape Canaveral	LC 3	16.1	Low-angle atmospheric flight over 320 km range
Bumper-7	29 July 1950	Cape Canaveral	LC 3	16.1	Low-angle atmospheric flight over 320 km range
51	31 August 1950	White Sands	Pad 33	136.4	Blossom 7- Nominal performance.
61	26 October 1950	White Sands	Pad 33	8	Explosion at 50s at Mach 3 terminated flight
H-II # 3	11 November 1950	White Sands	Pad 33		3rd and Final Hermes II test
1951
54	18 January 1951	White Sands	Pad 33	1.6	Stalled on pad for 13s then rose slowly for 38s before exploding
57	8 March 1951	White Sands	Pad 33	3.1	Blossom 8 - Three explosions at 15.5; 18.5 and 19.5s destroying til section
55	14 June 1951	White Sands	Pad 33	0	Exploded on pad at start of main-stage thrust after rising 6-inches
52	28 June 1951	White Sands	Pad 33	5.8	Blossom 9 - Tail explosion at 8s and then cut-off signal given at 22s.
TF-1	22 August 1951	White Sands	Pad 33	213.4	Army training test (last 5 launches by "Broomstick Scientists")^[16]^[17]
60	29 October 1951	White Sands	Pad 33	140.9	Army training test. Payload released but damaged on impact.
1952
59	20 May 1952	White Sands	Pad 33	103.5	Army training test. * Also designated TF-2
TF-3	22 August 1952	White Sands	Pad 33	78	Army training test. Thrust decreased after 53s. Tail separation at 217s.
TF-5	19 September 1952	White Sands	Pad 33	27	Army training test. Tail explosion at 27s terminating thrust.

Launches of Russian replicas of V2

Rocket number	Date	Launch site	Range	Remarks
T-01	18 October 1947	Kapustin Yar	207	Vehicle disintegrated at atmospheric reentry
T-02	20 October 1947	Kapustin Yar	231	Deviated 181 kilometres from intended flight path
T-03	23 October 1947	Kapustin Yar	29	Observation of vehicle was hampered by low cloud cover. Vehicle disintegrated, possibly due to the warhead failure.
T-04	28 October 1947	Kapustin Yar	29	Success
T-05	31 October 1947	Kapustin Yar	2	Started rolling after lift-off and crashed
T-06	2 November 1947	Kapustin Yar	260	Success
T-07	2 November 1947	Kapustin Yar	260	Lost fins after launch
T-08	4 November 1947	Kapustin Yar	268	Success
T-09	10 November 1947	Kapustin Yar	24	Control failure
T-10	13 November 1947	Kapustin Yar	270	Broke-up upon re-emtry. Landed within 180m of target.
T-11	13 November 1947	Kapustin Yar	270	Launched 5-hours after previous rocket and landed within 700m of target

Rocket destination

V = Versuchsmuster (English: Test/Experimental Type)
MW serial rocket from Mittelwerk)