The first A-4 flight-test model was completed 25 February 1942,[2] but slipped out of its "corset" after being fully tanked at Test Stand VII, fell 2 meters, smashed three fins, and came to rest on the rim of the engine nozzle.[1]: 158 After being repaired and renamed Versuchsmuster 1 (V1: Experimental Type 1),[3]: 9, 41 [4] the rocket failed during a test firing (witnessed by Albert Speer) and was scrapped
After being photographed by a British Supermarine Spitfire on 15 May, the second flight test model was damaged during its fourth firing test on 20 May, and then at the launch (observed by Speer, Erhard Milch, Fromm, Leeb, Witzell); a roll-rate gyro malfunctioned immediately after launch.[1]: 161–2 After the rolling missile became supersonic, the propellant feed system failed, telemetry ended at 54 sec (15000 ft), and the missile fell cart-wheeling into the Baltic less than a kilometer[5] away and exploded.[6][7]
Too steep due to pitch program error, otherwise success. Altitude 85 – 90 km - approximately the Kármán line altitude (85 ~ 100km), where aerodynamic lift vanishes. It was described at the time as the first rocket to reach the edge of space,[8][9] though not according to the modern FAI definition of 100km altitude. However, both the physical Kármán line and jurisdictional FAI definitions were made much later.
V-5
21 October 1942
84
147
P-VII
Steam generator misbehaved
V-6
9 November 1942
54
14
P-VII
Vertical, height 67 km
V-7
28 November 1942
37
8.6
P-VII
Tumbled, lost vanes
V-9
9 December 1942
4
0.1
P-VII
Hydrogen peroxide explosion
1943
V-10
7 January 1943
-
0
P-VII
Explosion on ignition
V-11
25 January 1943
64.5
105
P-VII
Too steep, rolled
V-12
17 February 1943
61
196
P-VII
Too shallow
V-13
19 February 1943
18
4.8
P-VII
Fire in tail
V-16
3 March 1943
33
1.0
P-VII
Vertical, explosion
V-18
18 March 1943
60
133
P-VII
Too steep, rotated
V-19
25 March 1943
28
1.2
P-VII
Tumbled, exploded
V-17
3 April 1943
64.5
?
P-VII
V-20
14 April 1943
66
287
P-VII
Fell on land
V-21
22 April 1943
59
252
P-VII
Fell on land
V-22
14 May 1943
62
250
P-VII
Cut-off switch failed
V-26
26 May 1943
66.5
265
P-VII
The Kommission für Fernschießen (English: Commission for Long-Range Firing/Weapons/Bombardment), including Albert Speer, Karl Dönitz, and Erhard Milch[3]: 45 [10]—viewed two successful Peenemünde A-4 launches (V26 around noon, V25 late afternoon),[1]: 190 followed by two launches of the V-1 flying bomb[11][12] (both V-1s plunged into the sea.)[5]
V-25
40
27
P-VII
Brennschluss (engine cut-off) at 40 s
V-24
27 May 1943
55
138
P-VII
-
V-23
1 June 1943
62
235
P-VII
Premature engine cutoff
V-29
11 June 1943
63.5
238
P-VII
-
V-31
16 June 1943
60.5
221
P-VII
Premature engine cutoff
V-28
22 June 1943
62.5
75
P-VII
exploded after 75 s
V-30
24 June 1943
65.1
287
P-X
Cut-off switch failed, first launch on Prüfstand X
V-36
26 June 1943
64.9
235
P-VII
-
V-38
29 June 1943
15
3
P-VII
Fell on airport
V-40
63.6
236
P-VII
Impact not observed
V-33
1 July 1943
-
0
P-VII
Engine cutoff at take-off, exploded
V-41
9 July 1943
4
0.1
P-VII
Fell on pump building
V-34
-
0
P-VII
Engine cutoff at take-off, exploded
V-54
12 August 1943
64
?
P-VII
Successful launch
V-49
6 October 1943
68
?
P-VII
Successful launch, duration 272 s; first launch after raid on 17 August 1943
V-71
15 October 1943
?
?
V-67
21 October 1943
?
?
V-69
25 October 1943
63
?
P-VII
Successful launch, duration 286 s
V-43
9 November 1943
?
?
V-73
4 December 1943
63
?
P-VII
Successful launch, duration 286 s
V-60
10 December 1943
69
?
P-VII
Successful launch, duration 247 s
V-59
21 December 1943
33
?
P-VII
Only partial success, premature engine cutoff, duration of flight 104 s
V-91
30 December 1943
?
?
January 1944
V-32
7 January 1944
43
?
P-VII
Exploded 43 s after launch
V-82
11 January 1944
?
?
V-77
20 January 1944
?
?
V-75
25 January 1944
?
?
MW 17003
27 January 1944
?
?
P-VII
First test of Mittelwerk-built rocket detonated three seconds after ignition without liftoff: "We just blew a million marks in order to guess what could have been reported accurately by an instrument probably worth the price of a small motorcycle." (Hartmut Kütchen, Engineer in Charge of Test Stand VII)[5]
February 1944
V-106
4 February 1944
?
?
MW 17009
9 February 1944
?
?
MW 17007
10 February 1944
?
?
MW 17010
11 February 1944
?
?
MW 17001
13 February 1944
?
?
V-98
15 February 1944
?
?
MW 17004
16 February 1944
?
?
P-VII
V-85
17 February 1944
?
?
MW 17021
18 February 1944
?
?
MW 17006
21 February 1944
?
?
MW 17011
23 February 1944
?
?
MW 17015
?
?
P-VII
V-112
28 February 1944
?
?
March 1944
V-84
2 March 1944
?
?
P-VII
Exploded
MW 17016
4 March 1944
?
?
V-151
7 March 1944
?
?
V-126
?
?
MW 17020
9 March 1944
?
?
P-VII
V-116
10 March 1944
?
?
V-128
?
?
V-88
11 March 1944
59
?
P-VII
Flight duration 282 s
MW 17022
15 March 1944
?
?
MW 17018
16 March 1944
?
?
MW 17033
18 March 1944
?
?
V-145
21 March 1944
?
?
V-121
23 March 1944
?
?
MW 17031
24 March 1944
?
?
MW 17019
27 March 1944
?
?
V-132
29 March 1944
?
?
April 1944
MW 17098
3 April 1944
?
?
P-VII
V-86
5 April 1944
?
?
P-VII
exploded after 17s
MW 17043
7 April 1944
?
?
P-VII
MW 17063
14 April 1944
?
?
P-VII
MW 17108
20 April 1944
?
?
P-X
May 1944
MW 17200
10 May 1944
?
?
P-X
V-152
12 May 1944
?
?
MW 17320
14 May 1944
?
?
V-136
16 May 1944
65
?
P-VII
MW 17323
17 May 1944
?
?
V-144
22 May 1944
?
?
P-VII
MW 17312
23 May 1944
?
?
V-89 MW 17309
24 May 1944
?
?
P-X
Launch Sequence #89:[13] Beginning with launching 89, temperature measurements at the tip of the rocket were used for diagnosing the airburst problem.[14]
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 tail 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")[18][19]
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 V2 by Soviet Union
The USSR captured the V-2 production facility at Nordhausen and assembled their own V-2s. Subsequently, they moved the equipment to the USSR and developed their own copy, the missile R-1.
Rocket number
Date
Launch site
Range (km)
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-entry. Landed within 180 m of target.
T-11
13 November 1947
Kapustin Yar
270
Launched 5 hours after previous rocket and landed within 700 m of target.
Notes and references
^1 The rocket designation "V" is for Versuchsmuster (German: Test/Experimental Type).[4]
^2 The rocket designation "MW" is for rockets produced at the Mittelwerk.
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