| Technical data | |
|---|---|
| Type | Yak-25RV-I (-II) |
| Function | target drone |
| Year | 1960 |
| Crew | 1 (none for Yak-25RV-II) |
| Engines | 2*3250/3900kg R-11B-300 |
| Length | 15.93m |
| Height | ?m |
| Wingspan | 23.4m |
| Wing area | 55m2 |
| Empty weight | 6285kg |
| Loaded weight | 9935kg |
| Wing Load (kg/m2) | 181 |
| Thrust to Weight |
1,53 |
| Speed at ?m | 900km/h |
| Range | 2500km |
| Ceiling | 20500m |
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Development of high altitude target drones based on Yak-25RV started in 1958, even prior trials of the experimental reconnaissater. Yak-25RV-I was intended as manned target for fighter-interceptors, practicing unarmed interception of high altitude targets. Difference from series Yak-25RV by deleted photoequipment. There were no surprises during trials (finished in 1961), and limited series production started in Ulan-Ude.
Minor improvements, introduced during production, resulted in 240kg weight savings, what was quite substantial for high altitude performance (August 1962).
If necessary, Yak-25RV-I could be re-equipped for unmanned operation. Standard unmanned version was designated Yak-25RV-II and was used by high altitude interceptor regiments for life firing practice. Yak-25RV-II was equipped with P-28 autopilot and remote control set. It was guided by specially modified Yak-30 trainer.
Retired reconnaissaters Yak-25RV were also converted into target drones.
| Predecessors | Modifications |
|---|---|
![]() Yak-25RV |
None |
| References | Links |
|---|---|
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| Created June 24, 1999 | Back to Main Gate |