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9 August 2003 yr. Was made flying test of experimental engine "XE-1 ". As a flight construction the sheaf of engine "XE-1 " with a plastic rod has been used. Length of a rod 80 cm, diameter of 8 mm. Weight of a rod 100 g. Weight of the engine with fuel 300 g. As directing the aluminium tube in which was used was inserted a rod connected with the engine. After start of the engine, it has quickly left on an operating conditions. The flight construction with greater acceleration has directed up. After the termination of work of the engine the flight construction became indiscernible on a background of the sky and has been lost sight. Searches of a flight construction on district have appeared unsuccessful. Height of flight to define it was not possible. |
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17 August 2003 yr. Start of a rocket "MAG-01-1" is made. The case of a rocket from PVC of a pipe in diameter 40ìì. And length 23 cm. The rocket had 4 stabilizers from plastic thickness of 1,5 mm. Nosecone demountable from a drawing paper. Start with system of rescue and an electronic sound beacon was originally planned, but at the last minute because of malfunctions in the scheme has been decided to start a rocket without these systems. For preservation of stability of a rocket in it has been placed equivalant of weights of the removed equipment. After start of the engine, the rocket has vigorously descended with directing. The active site last 1-1,5 sec. The height of flight has made approximately 250 m. Because of an initial inclination directing and a strong wind the rocket has departed on a parabolic trajectory. In current of all flight the rocket was well visible and has been lost track only during the moment of achievement of tops of trees of the next wood. Distance from a place of start up to a place of falling about 200-250 m. The rocket is not found.
Before launch 17 August 2003yr. |
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7 September 2003 yr. Start of a rocket "MAG-01-2" is made. The rocket differed from the progenitrix the advanced electronic part, changed configuration of parachutes, and as in the greater length of the case. Start of the engine managed to be made only from 3-rd attempt - fuel take dampness. After start of the engine the rocket has too slowly descended with directing and has failed on the ground in 20 meters from a place of start. Most likely because of the dampened fuel the engine and could not leave on full draft. From impact with the ground the design of a rocket and an electronic part have received insignificant damages. |
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7 September 2003 yr. Start of a rocket "MAG-02-1" is made. The rocket has been developed for engines of a series "MRE 10-10-4". The case and demountable nosecone have been made of a drawing paper. Stabilizers from the processed pieces from a wooden ruler. As a parachute the truncated garbage bag has been used. Slings from combined four times strings. Start of the engine can execut only from 2-nd time. As it has appeared an internal surface of the channel in fuel it is protected by a covering. After the sheeting has been scratched out and ignition the engine has been repeatedly made was started also a rocket quickly fly upwards, but on an inclined trajectory. In view of the small sizes it was possible to observe of a rocket only during work of the engine, tracing it on a smoke loop. Then, for some time, the rocket has been lost track. But after operation a ejection charge and disclosing of a parachute the rocket again became observable. Unfortunately because of the big range of flight and a strong wind a rocket has taken down in a place where it was difficult to reach and difficultly to search. Despite of all diligence the rocket has not been found. |
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14 September 2003 yr. Start of a rocket "MAG-02-2", analogue "MAG-02-1" is made. The rocket, after start of the engine, with very big speed has departed on an direct vertical trajectory. In some seconds the rocket has been lost track on a background of the sky. For any reasons the parachute has not been opened, the rocket during decrease has not been found out and to find it it was not possible. |
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21 December 2003 yr. Start of a rocket "MAG-02-3" is made. The rocket, after start of the engine, with greater acceleration has directed upwards. At height approximately 30 meters from a rocket it was separated nosecone and a parachute. The majority a sling at a parachute has been torn off. The case of a rocket, and also nosecone with a parachute have landed on small distance from each other. After survey of a rocket has been found fireout in cases of engine "MRE-10-10-4 " and the rocket. The reason of premature shooting nosecone with a parachute was break of gases between cases of the engine and a rocket. Breakage a sling has occured from strong aerodynamic impact at disclosing a parachute during an active site of flight of a rocket. |
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5 March 2004 yr. Start of the rocket "ASTRA-APOLLO-01" within the joint project "ASTRA" is made. On the given rocket engine "RMG-2" has been used. The system of rescue at the given stage of tests is not stipulated. After start of the engine, through 0,5 sec., there was a shooting of nozzle. Therefore the rocket could not reach height of 100-120 m., and has risen only on 30 m. Shooting of nozzle was consequence of the simplified technology of attachment of nozzle. On the given copy of the engine apertures in walls of the case as on the first test engine where got epoxy glue and by that more reliable attachment of nozzle was provided have not been made. At a turn of a rocket on a trajectory of descent from it was separated nosecone. At the further falling the rocket has touched branches of a tree that has led to deformation and partial separation of two stabilizers.
Before the first start of a rocket "ASTRA-APOLLO-01". 5 March 2004yr.
One minute readiness "ASTRA-APOLLO-01". 5 March 2004yr.
"ASTRA-APOLLO-01" has left on the ground only clubs of a smoke 5 March 2004yr.
"ASTRA-APOLLO-01" on a place of a landing 5 March 2004yr. |
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5 March 2004 yr. Start of the "MAG-02-3" rocket is made. The rocket, after start of the engine, with greater acceleration has directed upwards. At height approximately 200 meters the parachute has revealed. Therefore a strong wind at height and the small sizes of a rocket, it has been quickly lost on a background of the sky. Searches of a rocket have not crowned success.
"MAG-02-3" with the her founder 5 March 2004yr.
"MAG-02-3" before the start 5 March 2004yr.
Rise on "MAG-02-3" 5 March 2004yr. |
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5 March 2004 yr. Secondary start of the rocket "ASTRA-APOLLO-01" within the joint project "ASTRA" is made. The rocket, after start of the engine, with greater acceleration has directed upwards. At height approximately 15 meters the rocket has started to be shaken strongly, and then the trajectory of flight became chaotic. Right after it, from a rocket it was separated nosecone and all stabilizers. Then the rocket having stopped rise has fallen. Rocking of a rocket as it has appeared, has been caused by fifeout walls of the engine in the nozzle region of engine.
There is a preparation for the second start "ASTRA-APOLLO-01" 5 March 2004yr.
"ASTRA-APOLLO-01" again on start 5 March 2004yr. |
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10 April 2004 yr. Test start of a rocket "ASTRA-APOLLO-02" within the joint project "ASTRA" is made. This and the subsequent starts lead to this day were spent with the purpose of test of 4 remained engines RDG-2 made simultaneously with what were tested 5 March 2004 yr. After start the engine long reached a mode, then there was a shooting of bulkhead therefore that a rocket has flied up on height about 30 m. Probably on such outcome strong humidity, and also insufficiently reliable fastening of bulkhead has affected. Videorecording of start: astra1.avi 3.25Mb
Before the first start "ASTRA-APOLLO-02" 10 April 2004yr. |
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10 April 2004 yr. Secondary start of the rocket "ASTRA-APOLLO-02" within the joint project "ASTRA" is made. After start the engine and could not develop sufficient draft. The rocket has only risen on directing. Most likely a bad role rainy weather though engines were inserted into rockets directly ahead of start-up again has played, and were stored in a polyethylene package. Videorecording of start: astra2.avi 1.40Mb |
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10 April 2004 yr. The third start of the rocket "ASTRA-APOLLO-02" within the joint project "ASTRA" is made. In the engine which was used for this start there was a little change in a design of fastening nozzle and head. For reliability of their fastening in the paper case have been done on 4 apertures from each edge. At put epoxy glue it became numb in these apertures providing the best fastening of the future head and nozzle. After start the engine at once has left on a mode. The rocket with greater acceleration has descended with directing. At height approximately 15 meters the rocket has started to move on a spiral trajectory. At survey of a rocket after a landing have been found two fireout holes. Most likely it is necessary to increase thickness of head. Videorecording of start: astra3.avi 1.86Mb |
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10 April 2004 yr. Test start of the rocket "ASTRA-APOLLO-03" within the joint project "ASTRA" is made. After start the engine has quickly left on a mode and the rocket with greater acceleration has directed upwards. At height approximately 5 meters from a rocket was separate the engine. Test starts of rockets with engines RMG-2 have revealed necessity of completion of technology of their manufacture. Videorecording of start: astra4.avi 1.86Mb |
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8 May 2004 yr. Start of a rocket "MAG-01-2" is made. The design of a rocket has been as much as possible facilitated. The purpose of start was acquaintance with work of the purchased engine of the Polish manufacture. Flight of a rocket passed unstably because of strong displacement of the centre of gravity in area of a tail after unloading nose parts of a rocket. Videorecording of start: 0805mag2.avi 4.32Mb Videorecording of start(short): 0805ma2.avi 1.51Mb
Before start "MAG-01-2" 8 May 2004yr.
On a place of a landing "MAG-01-2" 8 May 2004yr. |
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8 May 2004 yr. Start of a rocket "MAG-03-1" is made. The basis of the case of a rocket was made by three aluminium banks from under beer. Engine MRE 10-10-4. Because of a strong wind and insufficient stability the rocket has reached small height. Videorecording of start: 0805mag3.avi 6.36Mb Videorecording of start(short): 0805ma3.avi 1.18Mb
Before start "MAG-03-1" 8 May 2004yr. |
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9 May 2004 yr. Start of a rocket "MAG-01-2" is made. This time on a rocket engine OD-1 in which was used already at assembly has been inserted electric igniter, and an aperture of nozzle covered by hermetic. Not looking at high humidity in day of start the engine was started from the first time, that testifies to a true method are sewn up fuel from humidity. Strongly facilitated rocket has confidently enough flied up, but during any moment has turned over having continued to gain height by inertia. Nevertheless the overall objective of start has been reached. Puttying by hermetic of an aperture of nozzle for prevention to dampen fuel has appeared effective. Videorecording of start not has gone right.
On a place of a landing "MAG-01-2" 9 May 2004yr. |
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9 May 2004 yr. Start of a rocket "MAG-03-1" is made. For this start the nose part of a rocket has been a little weighted, that has immediately affected its stabilization. After start the rocket has gone against a wind which was very strong this day. Feature of the given rocket is shooting the engine during the moment of operation a ejection charge. The engine was used MRE10-10-4. On the future it should extend a parachute at shooting. In the first starts the system of rescue is not stipulated. Because small weight of the case, the rocket at a landing did not receive strong damages. Videorecording of start: 0905mag3.avi 2.82Mb Videorecording of start(short): 0905ma3.avi 832kb
On a place of a landing "MAG-03-1" 9 May 2004yr. |
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16 May 2004 yr. In Moscow in Beetsevsky park have passed joint starts of rockets together with others rocketmans. Personally by me it has been made 4 starts of models of rockets this day. On start I represented two rockets - "MAG--03-1" and "MAG--04-1". Both rockets have been started on two times. Videorecordings and a photo are presented below. Videorecording of first start "MAG-03-1" 16 May 2004yr. : 1605mag3.avi 4.65Mb Videorecording of first start "MAG-03-1" 16 May 2004yr. (short): 1605ma3.avi 1.53Mb
The rocket will start "MAG-03-1" 16 May 2004yr.
On a place of a landing "MAG-03-1" 16 May 2004yr. Videorecording of first start "MAG-04-1" 16 May 2004yr. : 1605mag4.avi 8.98Mb Videorecording of first start "MAG-04-1" 16 May 2004yr. (short): 1605ma4.avi 1.33Mb
On a place of a landing "MAG-04-1" 16 May 2004yr. Videorecording of second start "MAG-04-1" 16 May 2004yr. : 1605mag41.avi 5.42Mb Videorecording of second start "MAG-04-1" 16 May 2004yr. (short): 1605ma41.avi 1.11Mb Videorecording of second start "MAG-03-1" 16 May 2004yr. : 1605mag31.avi 2.48Mb Videorecording of second start "MAG-03-1" 16 May 2004yr. (short): 1605ma31.avi 1.59Mb |
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11 August 2004 yr. With the equipment for registration of accelerations start of rocket MAG-03-2 is made . On this rocket was the system of rescue is applied at which engine of type MRE10-10-4 should was to separate and to pull out behind itself a parachute from a tail part of a rocket. The given system has not worked, because that electronics has been damaged at falling on the ground. Data have been lost. The scheme of the equipment in section "Onboard equipment" |
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17 August 2004 yr. With the equipment for registration of accelerations restart of rocket MAG-03-2 is made. On this rocket the same system of rescue, as during the previous start has been applied. The given system has not worked, because that electronics has been damaged at falling on the ground. Data yet not download that at impact about the ground the scheme has been destroyed. It is possible to draw a conclusion that it is necessary to finish the new scheme of system of rescue. The photo and video are presented below.
The rocket will start "MAG-03-1" 17 August 2004yr. Videorecording of second start of "MAG-03-2" 17 August 2004yr. : 170804s.avi 2.62Mb |
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21 August 2005 yr. Start of rocket MAG-02-4 with a sound beacon is made. Unfortunately on start nozzle of engine MRE10-10-4 was separated. Videorecording of start "MAG-02-4" 21 August 2005yr. : 21082005.avi 584 kb Videorecording of landing "MAG-02-4" 21 August 2005yr. : 210820051.avi 3.18 Mb |
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23 August 2005 yr. Start of rocket MAG-02-4 with a sound beacon is made. The system of rescue has not worked - the parachute has not revealed. Nevertheless the sound beacon has helped with search of a rocket. Videorecording of start "MAG-02-4" 23 August 2005yr. : 23082005.avi 484 kb Videorecording of landing "MAG-02-4" 23 August 2005yr. : 230820051.avi 2.47 Mb |
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26 August 2005 yr. The next start of rocket MAG-02-4 with a sound beacon is made. The system of rescue has not worked - the parachute has not revealed. Nevertheless the sound beacon has helped with search of a rocket. Videorecording of start "MAG-02-4" 26 August 2005yr. : 26082005.avi 584 kb |
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3 June 2007 yr. Test start of rocket MAG-05-1 with a videocamera is made. During flight parameters of a design, work of separate system of rescue, and also quality of work of the equipment were checked. By results of test start are drawn conclusions: 1. It is necessary to reduce the sizes or to refuse absolutely stabilizers for rockets with a videocamera. Otherwise because of complexities in maintenance direction of stabilizers there is a rotation of the case of a rocket with the chamber. 2. It is necessary to apply the directed reception antenn to increase in range of a radio channel. 3. At record of video which was made on laptop, it is necessary to close not used programs working in a background mode. Non-observance of it leads unsynchronization video and a sound.
The rocket will start "MAG-05-1" 3 June 2007yr. Videorecording of start "MAG-05-1" 3 June 2007yr. (onboard camera): 07.06.03.avi 4,34 Mb Videorecording of start "MAG-05-1" 3 June 2007yr. (ground camera): 07.06.03gr.avi 4,98 Mb |
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10 June 2007 yr. The next start of rocket MAG-05-1 with a videocamera is made. From a rocket stabilizers for elimination of an aerodynamic twisting have been dismantled. Unfortunately because of small length directing the rocket at start has not had time to type due speed for the stabilized flight that has led to chaotic deviations from a longitudinal axis.
Videorecording of start "MAG-05-1" 10 June 2007yr.(onboard camera): 07.06.10.avi 1,36 Mb |
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7 September 2008 yr. The next start of rocket MAG-05-1 with a videocamera is made. From a rocket stabilizers for elimination of an aerodynamic twisting have been dismantled. Regardless of the fact that the length directing has been considerably increased flight of a rocket was unstable. Videorecording of start "MAG-05-1" 7 September 2008yr.: 08.09.07.avi 2,73 Mb |
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29 May 2009 yr. The next start of a rocket "MAG-02-UE" is made. This rocket designed for engines of the Ukrainian manufacture 10-8-2. The rocket has flied up confidently enough. Height of rise about 300 m. the Engine has fulfilled perfectly. Videorecording of start "MAG-02-UE" 29 May 2009yr.: 09.05.29.avi 3,95 Mb |
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12 and 13 August 2009 yr. Trial starts of model of a rocket "ÌÀÃ-06" are made. That purchased engines of old Soviet manufacture MRE-2,5 have already become outdated the model of a rocket has departed normally only with 3-th time. In first two starts knocked out nozzle of engines. The sound beacon placed onboard, has helped with search of a rocket.
Before launch "ÌÀÃ-06" 13 August 2009yr. Videorecording of start "ÌÀÃ-06" 13 August 2009yr.: 09.08.13.avi 4,81 Mb |
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15 August 2009 yr. On joint starts of models of rockets "RocketFest" starts of models of rockets "MAG-02-UE" and "MAG-06" have been made. The photo and video will be presented later. |
